WO1989006883A1 - Alternating sequential half duplex communication system - Google Patents

Alternating sequential half duplex communication system Download PDF

Info

Publication number
WO1989006883A1
WO1989006883A1 PCT/US1988/004621 US8804621W WO8906883A1 WO 1989006883 A1 WO1989006883 A1 WO 1989006883A1 US 8804621 W US8804621 W US 8804621W WO 8906883 A1 WO8906883 A1 WO 8906883A1
Authority
WO
WIPO (PCT)
Prior art keywords
communication
message
transceiver
signal
input
Prior art date
Application number
PCT/US1988/004621
Other languages
French (fr)
Inventor
Klein S. Gilhousen
Franklin P. Antonio
Irwin M. Jacobs
Lindsay A. Weaver, Jr.
Original Assignee
Qualcomm, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Qualcomm, Inc. filed Critical Qualcomm, Inc.
Priority to EP89902364A priority Critical patent/EP0417099B1/en
Priority to JP1502240A priority patent/JP2974350B2/en
Priority to JP89502240A priority patent/JPH03502392A/en
Priority to AU30597/89A priority patent/AU624120B2/en
Priority to DE3855894T priority patent/DE3855894T2/en
Publication of WO1989006883A1 publication Critical patent/WO1989006883A1/en
Priority to HK98107081A priority patent/HK1008130A1/en

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B1/00—Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/69—Spread spectrum techniques
    • H04B1/713—Spread spectrum techniques using frequency hopping
    • H04B1/7136—Arrangements for generation of hop frequencies, e.g. using a bank of frequency sources, using continuous tuning or using a transform
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/10—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type
    • G02B6/12—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind
    • G02B6/12007—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings of the optical waveguide type of the integrated circuit kind forming wavelength selective elements, e.g. multiplexer, demultiplexer
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/26—Optical coupling means
    • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
    • G02B6/293—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means
    • G02B6/29304—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means operating by diffraction, e.g. grating
    • G02B6/29305—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means operating by diffraction, e.g. grating as bulk element, i.e. free space arrangement external to a light guide
    • G02B6/2931—Diffractive element operating in reflection
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/26—Optical coupling means
    • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
    • G02B6/293—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means
    • G02B6/29304—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means operating by diffraction, e.g. grating
    • G02B6/29316—Light guides comprising a diffractive element, e.g. grating in or on the light guide such that diffracted light is confined in the light guide
    • G02B6/29325—Light guides comprising a diffractive element, e.g. grating in or on the light guide such that diffracted light is confined in the light guide of the slab or planar or plate like form, i.e. confinement in a single transverse dimension only
    • G02B6/29328—Diffractive elements operating in reflection
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/26—Optical coupling means
    • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
    • G02B6/293—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means
    • G02B6/29379—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means characterised by the function or use of the complete device
    • G02B6/2938—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means characterised by the function or use of the complete device for multiplexing or demultiplexing, i.e. combining or separating wavelengths, e.g. 1xN, NxM
    • G02B6/29382—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means characterised by the function or use of the complete device for multiplexing or demultiplexing, i.e. combining or separating wavelengths, e.g. 1xN, NxM including at least adding or dropping a signal, i.e. passing the majority of signals
    • G02B6/29383—Adding and dropping
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/42—Coupling light guides with opto-electronic elements
    • G02B6/4201—Packages, e.g. shape, construction, internal or external details
    • G02B6/4204—Packages, e.g. shape, construction, internal or external details the coupling comprising intermediate optical elements, e.g. lenses, holograms
    • G02B6/4206—Optical features
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/42—Coupling light guides with opto-electronic elements
    • G02B6/4201—Packages, e.g. shape, construction, internal or external details
    • G02B6/4246—Bidirectionally operating package structures
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/42—Coupling light guides with opto-electronic elements
    • G02B6/4201—Packages, e.g. shape, construction, internal or external details
    • G02B6/4249—Packages, e.g. shape, construction, internal or external details comprising arrays of active devices and fibres
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/42—Coupling light guides with opto-electronic elements
    • G02B6/4201—Packages, e.g. shape, construction, internal or external details
    • G02B6/4249—Packages, e.g. shape, construction, internal or external details comprising arrays of active devices and fibres
    • G02B6/425—Optical features
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/05—Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
    • H01S3/08—Construction or shape of optical resonators or components thereof
    • H01S3/08004—Construction or shape of optical resonators or components thereof incorporating a dispersive element, e.g. a prism for wavelength selection
    • H01S3/08009—Construction or shape of optical resonators or components thereof incorporating a dispersive element, e.g. a prism for wavelength selection using a diffraction grating
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S5/00—Semiconductor lasers
    • H01S5/10—Construction or shape of the optical resonator, e.g. extended or external cavity, coupled cavities, bent-guide, varying width, thickness or composition of the active region
    • H01S5/14—External cavity lasers
    • H01S5/141—External cavity lasers using a wavelength selective device, e.g. a grating or etalon
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B10/00—Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
    • H04B10/50—Transmitters
    • H04B10/501—Structural aspects
    • H04B10/506—Multiwavelength transmitters
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/204—Multiple access
    • H04B7/212—Time-division multiple access [TDMA]
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L5/00—Arrangements affording multiple use of the transmission path
    • H04L5/14—Two-way operation using the same type of signal, i.e. duplex
    • H04L5/16—Half-duplex systems; Simplex/duplex switching; Transmission of break signals non-automatically inverting the direction of transmission
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24—Coupling light guides
    • G02B6/26—Optical coupling means
    • G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
    • G02B6/293—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means
    • G02B6/29331—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals with wavelength selective means operating by evanescent wave coupling
    • G02B6/29332—Wavelength selective couplers, i.e. based on evanescent coupling between light guides, e.g. fused fibre couplers with transverse coupling between fibres having different propagation constant wavelength dependency
    • G02B6/29334—Grating-assisted evanescent light guide couplers, i.e. comprising grating at or functionally associated with the coupling region between the light guides, e.g. with a grating positioned where light fields overlap in the coupler
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S5/00—Semiconductor lasers
    • H01S5/40—Arrangement of two or more semiconductor lasers, not provided for in groups H01S5/02 - H01S5/30
    • H01S5/4025—Array arrangements, e.g. constituted by discrete laser diodes or laser bar
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S5/00—Semiconductor lasers
    • H01S5/40—Arrangement of two or more semiconductor lasers, not provided for in groups H01S5/02 - H01S5/30
    • H01S5/4025—Array arrangements, e.g. constituted by discrete laser diodes or laser bar
    • H01S5/4031—Edge-emitting structures
    • H01S5/4062—Edge-emitting structures with an external cavity or using internal filters, e.g. Talbot filters
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S5/00—Semiconductor lasers
    • H01S5/40—Arrangement of two or more semiconductor lasers, not provided for in groups H01S5/02 - H01S5/30
    • H01S5/4025—Array arrangements, e.g. constituted by discrete laser diodes or laser bar
    • H01S5/4087—Array arrangements, e.g. constituted by discrete laser diodes or laser bar emitting more than one wavelength
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D30/00—Reducing energy consumption in communication networks
    • Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks

Definitions

  • the present invention relates to communication systems and more particularly to two-way telecommunication systems employing central message transmitting stations and Earth orbit relay satellites to transfer messages between mobile terminals and the central stations.
  • the invention further relates to a two-way telecommunication system using a sequential, alternating, half duplex communication pattern to reduce complexity and power requirements for each terminal while providing reliable communications between a large number of mobile system users.
  • Radio telephone, cellular telephone, and portable radio transceivers are all capable of providing some form of communication between a mobile transceiver and a base unit.
  • CB portable radio transceivers
  • these communication systems suffer from several drawbacks and have proven inadequate as message communication systems for serving a large number of widely dispersed users.
  • Direct communication, non-cellular, using traditional mobile radio transceivers also requires constant monitoring of a variety of frequencies all of which are crowded with existing traffic. These services, like cellular telephone, are subject to frequent system overload and signal degradation from several interference sources which makes them incapable of handling a large volume of traffic. These transceivers also have a low range imposed by the need to prevent interference with other communication systems.
  • What is needed is a communication system that allows continuous delivery of messages and related communication parameters or control information to a large number of users over a large geographical area.
  • the system needs to provide a return link for message acknowledgment and responses.
  • a system that allows the development of a complete private digital data network.
  • the system needs to be cost effective, simple to operate, maintain, and install, and minimize antenna requirements.
  • the system should also automatically adjust to handle many transfer errors associated with a mobile environment.
  • An advantage of the present invention is that it provides a modulation scheme that provides performance comparable to a predetermined signal to interference ratio in any interference scenario encountered.
  • Another purpose of the invention is to use a novel modulation, coding, and multiplexing technique which allows an inexpensive two-way mobile terminal with a very small antenna suitable for use on a moving vehicle, to receive and transmit data reliably using a satellite repeater.
  • Yet another purpose of the invention is to provide a modulation and coding scheme that is implemented digitally, preferably as firmware in signal processing chips of the VLSI type and in microcomputers.
  • Another advantage of the present invention is that the communication signals can be more effectively screened from existing communication services.
  • Yet another advantage of the present invention is a high performance, cost effective, and flexible implementation. Still another advantage is that the present invention provides a modulation and coding scheme that allows mass production of circuits and modules to be used for the remaining analog functions for the mobile terminals.
  • An object of the invention is to allow flexibility in data transfer rates so that receivers of differing transfer rates or capabilities are efficiently accommodated in a single system.
  • a further advantage of the system that results from the latter object is that more energy per bit can be used to compensate for unequal downlink power density across large geographical areas.
  • a message communication system for sending messages between central communication stations and one or more mobile terminals through Earth orbital relay stations comprising at least one central communication station having a first transceiver for transmitting a first communication signal from the central station to one or more mobile terminals and at least one mobile terminal having a second transceiver for receiving the first communication signal and demodulating it, and for transmitting at a predetermined duty cycle for the second transceiver, a second communication signal to at least one of the central communication stations.
  • the preferred predetermined duty cycle over which the second communication signal is transmitted is about fifty percent of the second transceiver duty cycle. At the frequencies of interest the fifty percent duty cycle is on the order of 10 - 20 milliseconds in length.
  • the address information is in the form of terminal addresses where messages are designated to be sent.
  • the central communication stations employ a terminal assignment device which determines which terminals in the system a message is directed to and, accordingly, assigns a terminal address to the message; and a channel assignment device for assigning each message to at least one of the data channels for transmission.
  • An address controller transfers a terminal address and an associated data channel assignment onto one of the address channels in response to input messages intended for each terminal.
  • multiple addresses are designated or assigned to a message.
  • special group or all call addresses can be associated with each receiver to facilitate multiple receiver addressing with a minimum of address information when possible.
  • a message input control device is connected to the channel assignment device and receives digital messages and transfers them serially onto designated data channels in response to an assignment from the channel assignment device at a rate of one message per channel at a time.
  • the input message data is nominally transferred at a rate on the order of at least 5,000 bits per second.
  • the communication system applies Golay [24,12] block coding to the digital messages prior to transmission and applies a corresponding Golay [24,12] block decoding process to resulting symbol data when received.
  • the Golay coding generates digital symbol data at a rate on the order of 10,000 bits a second.
  • a checksum computation is performed on input digital messages with a series of bits being added to the end of the message for checksum verification by the receiver.
  • the operating frequency of the TDM communication signal is frequency hopped at differing rates between the forward and return links over a preselected number of frequencies to decrease the power density of communication signals.
  • a unique triangular waveform is used to modulate the RF carrier center frequency with a 2 MHz peak to peak amplitude and a period of 30.24 milliseconds. This causes a triangle wave power dispersal so that the forward link has the same interference characteristics as a single video carrier saturating the transponder so that no unacceptable interference is generated for satellites adjacent to or within 2° from the satellite 20.
  • the central communication station uses an input or conversion element to convert incoming message information from digital or analog sources into digital messages at a predetermined transfer rate on the order of 5,000 bits a second.
  • the digital messages are then used to modulate a carrier to form the desired communication signal.
  • the transmitter is connected to at least one narrow-beam antenna which directs communication signals to a preselected relay satellite.
  • the communication system of the present invention uses mobile terminals having small, portable, directable, narrow- beam antennas connected to a demultiplexer and other means for detecting, demodulating, and decoding the TDM communication signal so as to receive message data.
  • the mobile terminals take advantage of the alternating duty cycle for transmission and reception to monitor the parameters of received signals and use changes as a guide to alter return link signal characteristics.
  • the transceivers employ a single set of local oscillators for both transmit and receive functions.
  • Figure 1 illustrates an overall diagram of a communication system operating according to the principles of the present invention
  • Figure 2 illustrates an overview of the message encoding/decoding and channel multiplexing of communication signals used in the system of Figure 1;
  • Figure 3 illustrates a schematic representation of exemplary circuit functions employed in a transceiver for the system of Figure l;
  • Figure 4 illustrates a schematic representation of exemplary demodulator/modulator circuit functions employed in a transceiver for the system of Figure 1.
  • the present invention provides a method and apparatus for transferring messages between one or more remote, mobile terminals and a series of one or more central communication stations or Hubs.
  • the communication system provides this information transfer for a large number of users by using a Ti e Division Multiplexed (TDM) communication signal having message transfer channels and receiver address channels which are used in an alternating half duplex mode. That is, forward link and return link transmissions or reception for the central communications stations as well as mobile terminals alternate between a send and receive mode on a predetermined periodic basis to allow use of common elements in the up and down conversion chains as well as in the IF elements to minimize complexity and costs.
  • TDM Ti e Division Multiplexed
  • FIG. 1 An overview of a communication system operating according to the principles of the present invention is illustrated in Figure 1.
  • a communication system 10 is illustrated having a mobile terminal (not shown) mounted in a vehicle such as a truck 12.
  • the truck 12 represents any of a variety of vehicles whose occupants desire to obtain occasional or updated information, status reports, or messages from a central communication source.
  • truck drivers or various drayage personnel often have a need for ready access to messages for more efficient operation.
  • a reply message may prevent the need for further communications or may indicate a need for an additional instruction or updated message from new information provided by a vehicle driver.
  • a reply message may prevent the need for further communications or may indicate a need for an additional instruction or updated message from new information provided by a vehicle driver.
  • by providing for a return link of communication even if limited in content, it is possible to incorporate other features into the communication link such as simple message acknowledgment to provide verification of message receipt by the terminal whether or not the driver operates on the information.
  • Other automatic responses may also be configured into the operation of the transceiver such as location and vehicle status.
  • the return link allows a driver to enter messages such as a verification of time and delivery information, or a report on current position or other status information.
  • a message is transmitted to the truck 12 from a central transmission facility or terminal 14 referred to as a Hub facility.
  • the central terminal or Hub 14 can be placed at a location such as a trucking terminal or central dispatch office allowing lower cite costs and local, direct, access to transmission equipment for maintenance and system upgrade.
  • the Hub 14 is located in a remote location more ideally suited for low interference ground-to- satellite transmission or reception.
  • one or more system user facilities in the form of central dispatch offices, message centers, or communication offices 16 are tied through a telephonic, optical, satellite, or other dedicated communication link to the Hub 14.
  • a message or network management center 18 can be employed to more efficiently control the priority, access, accounting, and transfer characteristics of message data.
  • the Hub 14 or management center 18 can be interfaced to existing communication systems using well known interface equipment such as high speed modems or codecs which feed message signals into the communication system 10.
  • High speed data management computers can also be used to determine message priorities, authorization, length, type, accounting details, and otherwise control access to the communication system 10.
  • the Hub 14 employs an Extremely High Frequency (EHF) transceiver to establish an forward and return link or up and down link communication paths with a geosynchronous Earth orbiting relay or repeater satellite 20. These links are maintained at one or more of a number of preselected frequencies or frequency ranges.
  • EHF Extremely High Frequency
  • a typical satellite system employs a series of repeater transponders for transmitting 12 GHz frequency signals for TV or radio transmissions to ground stations.
  • the preferred embodiment of the communication system 10 employs uplink and downlink carrier frequencies in the EHF Ku band to allow access through the transponders on existing or new communication satellites already launched or planned.
  • the communication system 10 can take advantage of unused or excess satellite capacity at these frequencies and does not require the launching of its own, new, dedicated satellites. Therefore, the benefits of the present invention are immediately available without additional expensive satellite technology.
  • the communication system 10 can also be implemented at other frequencies dependent upon available satellite transponders and can provide improved communication through some ground based repeaters.
  • the Hub's transmission signal is transferred through a diplexer 22 to an antenna 26.
  • the antenna 26 comprises a very small aperture antenna for directing the communication signal 24 to a single orbiting satellite.
  • a forward link communication signal, designated 24a, is transmitted through the antenna 26 to the communications satellite 20 at the preselected uplink carrier frequency.
  • the communication signal 24a is received.by the repeater satellite 20 where it may be translated to a second frequency for the downlink transmission 24b.
  • the repeater satellite 20 where it may be translated to a second frequency for the downlink transmission 24b.
  • Those skilled in the art of communications understand the apparatus needed to perform this reception and conversion function which are known in the art. Using different frequencies for the uplink and downlink communication signals reduces interference.
  • the transmitted forward downlink signal 24b is received by a mobile transceiver 70 (Fig. 4) through a small, generally directional antenna 30.
  • the antenna 30 is constructed to have about 15 dB of gain and to be directional within a 40-50° elevation beamwidth and 6-10" azimuthal or orbital arc beamwidth.
  • the antenna 30 is mounted so that it is capable of being continuously rotated over a 360 degree arc and has an unobstructed filed of view for the satellite 20.
  • the antenna is connected to an antenna pointing and tracking control system 74 (Fig. 4) for tracking the satellite 20 as the vehicle 12 changes position relative to the satellite.
  • An exemplary antenna rotation mechanism is found in co-pending U. S. Patent Application
  • Messages, or message data are transferred into the Hub 14, or control station 18, where they are converted into digital message signals which at a rate on the order of 5,000 bits per second.
  • Messages can be received directly as digital data at various bit rates and accumulated or stored for translation to the desired system transfer rate.
  • messages are received as audio message signals that are keyed in by system operators to form the desired message signals.
  • some message information is generated internally or directly by the network management center 18 for communicating system type data, such as time, terminal assignments, rates, etc.
  • Each message signal can be subjected to a variety of coding, encryption, or error detection and correction schemes prior to transmission.
  • individual terminals can employ unique codes or ciphers to provide secure message delivery capabilities.
  • at least two encoding steps are implemented for all digital messages or message data.
  • One step comprises applying a system 10 checksum algorithm to the digital message data.
  • the checksum algorithm employs on the order of 30 bits of information to indicate the values resulting from checksum computations which are used to detect transfer errors.
  • An exemplary checksum formula for use in the communication system 10 is the computation of the polynomial: X 30 + X 29 + X 3 + X 2 + X + 1. When calculating this checksum the address field (see below) of a message is ignored so that channel addresses do not alter checksum values.
  • a second step comprises encoding all data, message, instructions, or addresses, using a Golay [24,12] block code to encode every 12 bit block of information, including checksum, type and recipient information, into 24 binary symbols for transmission. These 24 bits are then transferred at the desired system transfer rate.
  • Golay [24,12] block coding scheme means that 5,000 bits of message data forms a 10,000 bit encoded symbol stream for transmission. Therefore, the system 10 transmission signal rate is about 10,000 binary symbols or bits per second to accommodate the 5,000 bit per second input data rate.
  • the code symbols or blocks are decoded to regenerate the 12 bit blocks of information.
  • a Golay [24,12] or similar code acts to minimize transmission error by decreasing the impact of single bit errors on a data stream through spreading the data out over multi-bit patterns.
  • Each bit error affects only a fraction of a bit in the message which is effectively compensated for by the error correction schemes used until very high error rates occur.
  • the encoded message symbols are used to modulate a frequency generator or source such as a Direct Digital Synthesizer which creates an FM modulated carrier, at a preselected frequency which is up-converted to the desired EHF band for transmission to the satellite 20.
  • the encoded symbols can be used to drive a BPSK modulator which is coupled to the carrier wave source for the communication system 10.
  • each symbol is shifted in phase from the previous symbol, either -90" to indicate a 0 or +90° to specify a 1. This is referred to as Differential Advance Retard Keying and improves acquisition by the terminal because every symbol contains a phase transition.
  • TDM Time Division Multiplexed
  • the TDM approach divides the total transmitted (or received) spectrum into temporal increments or frames of predetermined length.
  • Messages or message signals transmitted in or by the communications system 10 are allocated portions of this time controlled sequence known as channels, and no other signal uses the system at exactly the same time.
  • the allocated portions or channels are very small, temporally, and their interleaving across successive frames very large so that communication appears simultaneous to all terminals.
  • Methods and apparatus for generating, transmitting, and controlling TDM signals are well known in the communication art and can be accomplished using a variety of signal multiplexing and control devices.
  • Each frame consists of a number of channels which represent substantially identical, sub-frame length periods during which symbols are transferred. This means that messages or message signals are transferred a few bits at a time during each successive frame until the message is completed.
  • the preferred embodiment divides each frame into 25 sub-frames or channels. However, those skilled in the art will readily understand that the number of channels depends on the transmitting speed of the communication system 10, number of users to be accommodated, and frequency hopping schemes as described below.
  • the communication system can accommodate packets of differing lengths between 4 to 256 characters each, depending on the type, burst rate, or size of messages being transferred.
  • the messages, preformatted or free-form are generally limited to 2000 characters in length to facilitate transfer speed and high message capacity.
  • Each packet is generally segmented into fields of information such as the type of message, typically a 6 bit entry to distinguish between possible alternative system formats, the length of the message, to allow proper tracking, the body of the message, and the checksum bits. There is also an address field of 24 bits associated with each message as discussed further below.
  • Those skilled in the art will readily understand that some "zero packing" will be used from time to time to assure a uniform frame size regardless of overlapping message lengths, varying packet sizes and transmission rates, or empty channels. However, unused channels generally will have random data transmitted to improve tracking and acquisition of channels by transceivers. To assure that each transceiver is tracking and demodulating a designated channel, a series of codes or code masks can be used with the data to detect tracking errors.
  • short bit patterns can be added to the data transferred by each channel to allow automatic differentiation from data in adjacent channels.
  • a transceiver commences demodulating one channel it records the code mask for that channel. The mask is used to decode or demodulate all data received until the end of the message. If the transceiver erroneously uses data from adjacent channels, the code mask will prevent incorporation into the message.
  • Frequency Hopping of the carrier frequency can be used.
  • An FH technique spreads the power density of the signal 24 over the entire transponder 48 MHz bandwidth, reducing downlink power density which minimizes interference with other communication services and provides processing gain which the transceivers use in rejecting the interference of other services.
  • the basic techniques of FH- TDM transmissions are known in the communication art and also provide a vehicle for spreading a signal out over a given bandwidth so that transmission errors caused by frequency selective fading or other aberrations only affect a small portion of the signal.
  • frequency hopping according to a unique pattern allows some degree of security for some system 10 users.
  • the forward link FH scheme comprises dividing the appropriate forward link (downlink) transponder bandwidth (11.7 - 12.2 Ghz) into 240 frequencies located approximately 2.5 MHz apart.
  • the hopping rate for the frequencies of interest is on the order of 200 frequencies per second covering the 240 discrete hopping frequencies before recycling. This means that the dwell time for each frequency is about 5 milliseconds. If each TDM frame is transmitted at a new frequency then each frame is about 5 milliseconds long and the size of each channel is roughly 0.20 milliseconds in length.
  • the frequency hop pattern can comprise a simple linear progression from high to low or vice versa, but a more complex pattern based on a pseudo-randomly generated frequency selection sequence is preferred.
  • a TDM signal without frequency hopping will benefit greatly from the method and apparatus of the present invention.
  • each frame period allows 2 symbols to be transmitted per channel. This would imply a transmission rate of forty-eight (48) code symbols every frame.
  • the preferred embodiment uses a fifty (50) symbol transmission rate for each frame with the first symbol period employed for settling time to assure that the transceiver has locked onto, and the transmitter is accurately within, the selected frequency and not offset due to the changing characteristics of the frequency source.
  • the second symbol is used as a phase reference for the third symbol in the stream of fifty symbols, with the third symbol being the first message symbol.
  • Each successive symbol is used as a phase reference for the next.
  • the code blocks or symbols are divided into alternating groups or sequences. That is, every other code block is selected and placed in one 24 symbol group for transmission. This separates every other code symbol from its adjacent symbol which spreads code symbols that are close together in code to be far apart in time. This interleaves the code blocks to provide a means of minimizing signal errors generated as a burst of errors in a sequence by spreading the message signal over a wide signal bandwidth.
  • the FH-TDM type communication signal 24a is transmitted by the Hub 14 through the repeater satellite 20 (where it becomes signal 24b) to all of the terminals within a given geographical zone or region serviced by the satellite.
  • This zone can be as large as an entire country, or as narrow as a small state depending on the application.
  • each ter inal in that zone normally would have to detect, monitor, and demodulate the signal 24b in order to receive messages. If the messages are simply applied across all of the channels, then each transceiver has to continuously track, demodulate, and decode the entire wide bandwidth signal to assure reception of a relevant message.
  • terminal selection is accomplished using a new terminal or transceiver addressing technique for TDM communication signals which comprises a two part addressing scheme. This technique is explained in greater detail in copending U. S. Patent Application SN.
  • each terminal is assigned a unique system address which is known to all Hub 14 transmitters or system management centers 18 used by the communication system 10.
  • the terminal address establishes an individual identity for each terminal in the system. This address is generally set at the time of terminal manufacture or installation and can be made unalterable by a transceiver user or made dynamically changeable by the system 10 depending upon the system requirements or costs.
  • the transceiver addresses are designated or determined by a 19 bit address term making approximately 524,288 (2 19) terminal addresses available which allows a very large number of users for the message communication system 10.
  • terminals can also respond to specialized "system" addresses such as a
  • A is 4 and D is 21.
  • other values for the total number of channels and address channels can be used depending upon specific system requirements.
  • the A address channels are used to transmit address information and designations for those terminals whose messages are being transmitted by the Hub 14.
  • the D data channels are used to transmit the messages for the designated terminals.
  • the transmission of each message address precedes the transmission of that message by a predetermined period of time to allow a terminal to adjust its, tracking circuitry and synchronize with the appropriate channel before the arrival of the message.
  • the address channels are typically designated as system channels 1, 2, 3, ... etc. However, these channels can be separated by data channels where channel tracking either permits or desires this spacing for transceiver demodulation.
  • the number of channels can be dynamically adjusted by the system 10 to accommodate several problem situations. One problem arises when there are a great number of messages, saturating the address channels but the messages are short, thus leaving excess data channel capacity. In this situation, a data channel could be reassigned to be an address channel. The opposite problem occurs when there are an average number of messages but they are all maximum length.
  • the system 10 may find it advantageous to use one of the address channels for data to decrease the number of messages being backlogged.
  • This addressing scheme means that address information only needs to be demodulated at a fraction of the communication signal rate allowing each transceiver to monitor the communication signal 28 at this lower rate until it detects its address.
  • the transceiver switches to the appropriate channel and begins demodulating and receiving the message. Therefore, it will be apparent to those skilled in the art that transceivers are not demodulating nor decoding the entire, or even a majority of the communication signals 28 transmitted by the communication system 10. This allows a less complex and slower speed reception circuit which reduces power and cost while increasing reliability and ease of construction.
  • each transceiver can be assigned a specific address channel to monitor, dynamically or fixed, which further reduces processing to a 1/N rate for both addressing and message demodulation.
  • an incoming communication signal comprising interleaved code symbols 50 is received by each transceiver on a series of signal channels 52 which are frequency hopped in a sequence of hops 54.
  • the messages are received on the data channels 56 while address information is received on the address channels 58.
  • the digital code symbols comprise the code block symbols described above and are received at a rate of two symbols per channel per frequency hop. There are two extra symbols received during each hop with the first disregarded or lost due to settling of the transceiver and the second being used to obtain the phase required to track the third symbol. Therefore, there are forty-eight information symbols per frame in each hop and 48 symbols received for each channel after 24 hops.
  • the output of the address channels 56 comprises 24 bit length information sequences 64 which use 19 bits to specify a transceiver address within the communication system 10 and 5 bits to indicate a channel selection for receiving a message directed to that transceiver.
  • Each message has an address 24 bit segment associated with it which is segregated from the message and transferred over the address channels to flag an appropriate transceiver.
  • the output of the message or data channels 58 comprises a series of successive 12 bit blocks 68 which comprise a header that indicates the type of message, including its length, a main body of the message and a series of checksum bits for error detection.
  • the length of the incoming message is important so that the transceiver can properly track the entire message or provide an indication of error if the entire message is not received.
  • address information for a transceiver is sent before the message is transmitted on a data channel.
  • the amount of "lead time" for transmitting address information depends on the channel switching speed of the transceivers as would be known by those skilled in the art.
  • the address must be provided prior to the message by a time period equal to this switching time plus some settling time for the transceiver to properly and accurately track the designated channel.
  • transceiver 70 for receiving and demodulating communication signals from the Hub 14 and satellite 20.
  • the transceiver 70 is connected to the antenna 30 through a diplexer 32 for receiving the satellite downlink signal 24b which is transferred into a demodulator 72 for demodulation into an encoded symbol stream (digital message) .
  • the demodulator 72 employs elements known in the art for down-converting the received communication signal 28 to a lower IF frequency level and then symbol frequency level (10K symbol bits per second) .
  • a local oscillator and other reference signal sources would be provided for mixing with the communication signal 24b along with one or more bandpass filters.
  • the demodulator 72 transfer rate is synchronized with the modulator used in the Hub 14 or the satellite 20.
  • Synchronization for the transceiver 70 is accomplished by tracking and synchronizing with the frequency hopping pattern of the communication signals. Once a transceiver ha ⁇ synchronized with the frequency hopping of the TDM signal frames then the internal frame timing is automatically detected as well.
  • the mobile transceiver or terminal 70 incorporates a low cost microprocessor or similar controller 74 for implementing signal processing, acquisition, and demodulation functions.
  • a low noise amplifier 76 and the conventional down-conversion chain of the demodulator 72 provide a signal to the microprocessor for signal acquisition, tracking and demodulation.
  • Information from the demodulator 72 or the microprocessor 74 is provided to an antenna tracking and pointing controller 78.
  • the antenna 30 is generally swept through a series of 360" arcs by the controller 78, until a signal is detected from the satellite 20, in the receiver's frequency range, above a predetermined threshold. At this juncture one or more tracking and signal processing algorithms are used to determine the direction of highest signal strength and the antenna tracks that direction relative to receiver or vehicle 12 position or movement.
  • a receiver address storage element 82 is connected to the demodulator 72 for storing the address assigned to the receiver 70 and used to determine the presence of a message from the satellite 20 or Hub 14.
  • the address storage element 82 typically comprises a small ROM or similar memory device connected to the microprocessor 74.
  • the address can be hardwired into the microprocessor structure itself such as in the case of scratch memory, or internal RAM although this may not be convenient or cost effective in many applications.
  • the use of a separate memory element allows alteration by service personnel at a future time where needed.
  • receiver address on a portable storage element such as a magnetic strip or cartridge which can be read by a card reader (not shown) connected to the microprocessor 74.
  • a card reader not shown
  • the channel designated by the corresponding address information is also received and registered by the receiver 70.
  • the receiver 70 automatically switches to synchronize reception on that channel and begins demodulating a message signal.
  • the antenna fails to track the communication signal 28 at any time during the reception of a message, or any type of signal failure or blockage occurs, one or more errors will be detected in signal demodulation and no message will be displayed. Such errors would could include premature termination of the message before the length, time, specified in the message header or the failure of the checksum verification process.
  • the demodulated communication signal is transferred to a decoder 80 where Golay decoding occurs.
  • a pseudo-random code source or other related code storage element 84 provides any necessary code sequences required to further decode a received message.
  • the decoded message bits may be temporarily stored in a memory element 86 before visually being displayed by a display element 88.
  • An exemplary display element comprises a two to four row, twenty to eighty character wide display unit capable of running from relatively low current.
  • the individual segments of the display can comprise LED, LCD, electroluminescent, or discharge element type character displays. Consideration must be given to the brightness generally required in a vehicle environment to prevent undue distraction of a drivers attention.
  • the display unit 88 should be as compact and lightweight as possible so that it can be mounted in an easily viewed location.
  • the display can incorporate a message ready indicator or message error indicator so that the receiver users knows that a message was sent.
  • the message can be interfaced to other processing elements, such as a portable computer, through an interface device or connector 92 or printed out by a hard copy device 90, such as a small thermal printer.
  • the communication system 10 offers the added advantage of a return communication link so that short responses can be made to received messages where desired.
  • each transceiver or mobile terminal uses a low power signal on the order of 1 Watt and an antenna gain of about 19 dBi for a transmit power of 19dBW.
  • the return link is transmitted at a higher frequency than the forward link to decrease interference.
  • the frequency chosen is in the typical satellite Ku band transponder range between 14-14.5 GHz. However, as before other frequencies can be employed for this return link.
  • the return link communications signal 28 uses a FH waveform similar to the forward link but takes advantage of typically slower data transfer rates occurring from a mobile communications terminal. That is, return messages or data are not going to be entered into a local terminal at high speeds where a terminal operator is manually responding to a message. Where acknowledge and other prestored signals are used they are adjusted to a slower bit rate to comport with the slower manual entry mode.
  • the FH rate needs to be decreased on the return link in order to allow sufficient dwell time for each channel to transmit the data.
  • Golay [24,12] encoded data this becomes 280 symbols per second. Therefore, the forward link rate of 200 frequencies per second should be reduced to about 60 frequencies per second.
  • the small, portable and directable antenna 30 typically has a beamwidth on the order of 6-10' , which is wide enough to encounter more than one satellite. Therefore, steps are taken to provide a return link waveform that does not interfere with existing services on adjacent satellites.
  • a direct sequence spread spectrum coding function is applied to the return transmission to spread the signal out over the transponder bandwidth and make the communication signal 28 appear as relative noise to adjacent services.
  • a short direct sequence pseudo-random code is used. This code is typically applied to a direct digital synthesizer or similar modulated frequency driver.
  • either the forward or return link communication signals are modified by modulation with a special modulation waveform that disguises the signal to other services.
  • the triangular modulation can be implemented by altering the characteristics of a DDS output which will accurately track a triangle wave and yet transfer more information than a true video signal.
  • the center frequency is fully synthesized at the Hub and mobile terminals and can be placed anywhere within the transponder, after informing the transceivers of the new center frequency. hile interference by the transceiver 70 with other services has been discussed, this is not the only restriction on optimum operation.
  • the transceivers 70 must also be able to quickly and reliably acquire the Hub 14 or satellite 20 transmissions and continue to track them while moving. In addition to interference from other systems, the transceivers 70 face interference and loss of signal due to a variety of inherent impediments for mobile communications, including doppler effects, frequency fading, etc.
  • the present invention counters many of these problems by assuming that there may be significant changes in the transmission capability of the communication system 10 on a very short time scale, interpreting any change to altered environmental conditions, and adjusting for such changes.
  • Each transceiver 10 monitors the quality of or results of communication with the Hub 14 and periodically adjusts operational parameters to maintain or improve communication links accordingly.
  • Transceivers are operated in a half-duplex mode with transmissions done at a 50 percent duty cycle to allow for continued antenna tracking and error correction based on received downlink signals.
  • any partial message is deleted from memory and not present for display.
  • the transceiver uses this information to recognize that there is no uplink. Actually an uplink may be possible and the error could be in the receiver only. However, the system assumes that without a downlink the uplink information is either not being received or is no longer needed. In any case, the transmitter function is terminated if the receiver link is terminated for any reason.
  • the transceiver 70 is normally configured to be in a receive mode wherein it monitors an assumed satellite position or general horizon looking for a signal for incoming communications signals. This initial signal acquisition occupies the full duty cycle of the transceiver. Once a signal is detected, tracked, and acquired, the transceiver operates on the 50 percent duty cycle. Each half cycle is a very short period of time on the order of 15 milliseconds.
  • the transceiver 70 After signal acquisition, the transceiver 70 synchronizes with the forward link FH pattern and rate and switches to the correct channel frequency for receiving either channel address or a message. Then, every 15 milliseconds the transceiver 70 switches to the return link FH rate and pattern and for 15 milliseconds. However, the transceiver does not transmit until or unless requested to do so by the Hub 14 or communications management center 18. This assures that the Hub is prepared to receive the message and that there are no higher priority tasks in progress, including receipt of high priority emergency messages or alternate system 10 operating data. Also, polling controls the number and frequency of receivers to regulate interference at all times. The transceiver 70 then returns to the receive mode and continues to demodulate and decode the message, if any, so forth.
  • This alteration between send and receive on a periodic and short term basis provides the transceiver 70 with several operational advantages.
  • the transceiver monitors the power level .and characteristics of received signals every 15 milliseconds and detects substantial changes.
  • the hub and mobile transceiver must agree well enough in terms of frequency to allow the transceiver to acquire and track the forward link signal.
  • the transceiver will search +/- 18KHz about the nominal specified frequency
  • the hub 14, satellite 20, management center 18, and transceiver 70 all have internal reference oscillators for establishing transmission frequencies employed. Each of these references can drift and cause frequency errors.
  • the satellite cause small frequency errors during translation of the communicaiton signals between up and down link frequencies.
  • the transceiver 70 reference oscillator may drift and is subject to temperature change induced variations.
  • the Hub employs a Forward Link Processor (FLP) which adjusts transmission frequencies to correct for some of the possible errors listed above.
  • FLP Forward Link Processor
  • Satellite translation error is measured and corrected by using a reference receiver at the Hub and using a testing or control pattern of information between the Hub and the reference receiver through the satellite.
  • the FLP sends commonads to the satellite to adjust the translation frequencies to match what the Hub transmits. Any residual error, say from the control signals, is also assumed to be too ⁇ al to have an impact on communication quality.
  • the transceiver oscillator drift is corrected by the transceiver according to a long term software program that assumes certain drift characteristics for the transceiver oscillator. Therefore, temperature drift is the largest reference error and it is corrected by comparison to the other references using the communication signals.
  • the transceiver assumes initial frequency variations in singals are due to initial frequency tracking and synchronization mis ⁇ alignment.
  • the receiver assumes that all variations are due to receiver positioning relative to the relay satellite or similar non-internal frequency problems. Therefore, the receiver assumes that antenna pointing and tracking must be adjusted when the overall power level of a signal decreases (as when a corner is turned) and that variations in frequency tracking are caused by doppler effects which must be countered. That is, variations in received frequency are assumed to be caused by changing characteristics of the communication link itself and not the error sources discussed above, which have been corrected.
  • the present invention provides improved tracking and Doppler compensation.
  • transceiver does not need a full compliment of circuitry to handle both functions. That is, several circuit elements can be shared between the two functions since they are separated in time. Elements such as the antenna, antenna and related circuit feed cables, certain bandpass filters, and the transceiver local oscillators can be shared between the transmit and receive functions if configured appropriately.
  • the transmit and receive frequencies are chosen to be within the preferred Ku or 11.5 to 14 GHz bandwidth as disclosed above.
  • one or more up-conversion stages or IF mixing stages are required in the transceiver 70 circuitry. It has been found that a series of desirable uplink and downlink or forward and return link frequencies within the specified bandwidth and FH scheme can be chosen so that they are separated by a very narrow margin in the intermediate IF stages and a common tunable local oscillator can be employed for both the transmit and receive function.
  • FIG. 4 A schematic diagram of a transceiver 70 analog modulation/demodulation section 100 operating according to the principles of the present invention is illustrated in Figure 4.
  • a modulator 100 is shown having a Fine frequency synthesizer 102 and a Coarse frequency synthesizer 104.
  • the coarse frequency synthesizer or Local Oscillator (L.O.) 104 represents a source of high to extra high frequency signals which is generally tunable over a broad range of interest in large steps on the order of 2-5 MHz each.
  • An exemplary coarse oscillator for use in the present invention is a Phase Locked Loop (PLL) type oscillator generating output signals at frequencies on the order of 652 - 1175 MHz. in Steps Of 2.5 MHz. (652.5, 655, 657.5,...)
  • PLL Phase Locked Loop
  • the fine frequency synthesizer or oscillator 102 provides a finely tunable source of frequency with very low noise and is tunable over a smaller frequency range and or in smaller discrete steps.
  • the fine frequency synthesizer 102 can comprise one of several frequency sources that provide a high accuracy, high resolution output in the frequency range between 5 to 20 MHz with direct digital synthesizers being preferred.
  • An exemplary circuit for an advanced digital synthesizer useful in the present invention is disclosed in U. S. Patent Application SN. , filed January , 1988 and assigned to the same assignee as the present application.
  • a single reference frequency source 106 is shown for use with the PLL of the coarse synthesizer 104, the fine synthesizer 102, other elements in the modulator/demodulator 100 and other oscillator and processing stages for the transceiver 70.
  • This provides a system wide, synchronized reference or clock source which improves signal to noise ratio and allows simplified system wide synchronization with other system where desired.
  • An exemplary reference source 106 provides a reference signal at 10 MHz from a highly stable reference source such as a rubidium standard.
  • Communication signals received from the hub 14 are received on the antenna 30 and transferred through an up/down converter 108 and through a band pass filter li ⁇ to a power splitter 112.
  • the power splitter 112 exhibits a 3db separation and is used to redirect received signals along a different internal processing path from the transmit signals and transfer them to a demodulation portion of the transceiver 70.
  • Incoming or received communication signals 24b are first mixed with the output of the coarse synthesizer 104 to down convert them to a lower IF freguency in the range of 250 + 7 MHz. This is accomplished using a signal mixer 114 which uses the communication signal as one input and the output of the coarse synthesizer 104 as a second input.
  • the output of the mixer 114 is filtered by a band pass filter 116 to remove unwanted frequency components added to the down-converted communication signal by the mixer 114.
  • the output of the band pass filter 116 is transferred to a second mixer 118 which has the output of the fine synthesizer 102 as one input.
  • the mixing of these two signals provides a final IF frequency signal in the 20 + 20 MHz range.
  • the output of the mixer 118 is transferred though a crystal filter 120 to the microprocessor 74 and subsequently decoded and displayed as a message for the transceiver 70.
  • a transceiver 70 user When a transceiver 70 user has input a message through the display unit 88 or similar input means it is encoded and transferred into the modulator/demodulator 100 by modulating the input of the fine synthesizer 102. This is easily accomplished using direct digital synthesizer technology as understood by those skilled in the art.
  • the output of the fine synthesizer 102 is applied to one input of a mixer 124 and the output of the coarse synthesizer 104 is applied to a second input of the mixer 124 to generate an intermediate IF frequency.
  • the resulting transmit carrier is transferred to the up/down converter 108 connected to the transceiver antenna 30.
  • the bandpass filter 104 filters unwanted frequency components from the transmit communication signal as it is transferred through the splitter 112 to the up/down converter 108.
  • the bandpass filter 110 is generally a single section varacter tuned voltage controlled type filter which removes local oscillator or synthesizer frequencies and low frequency images and also allows tuning to other frequency bands for use in the forward link demodulation.
  • the communication signal is up converted by the converter 108 to the desired 11.7 - 12.2 GHz range by mixing with 13.1 GHz reference.
  • the up/down converter 108 can be configured as an output channel having a power amplifier connected to a diplexer for the antenna 30 with a mixer 130 connected to a local oscillator providing the 13.1 GHz mixing reference frequency. On the return link the up/down converter 108 presents a second mixer connected to the 13.1 GHz local oscillator for down converting received communication signals.

Abstract

A message communication system employing one or more centralized communication stations (22) transferring messages through Earth orbit repeater satellites (20) to or from mobile terminals (10) with at least one central communication station having a first transceiver for transmitting a first communication signal to one or more mobile terminals and at least one mobile terminal having a second transceiver for receiving the first communication signal and demodulating it, and for transmitting at a predetermined duty cycle of the second transceiver, a second communication signal to at least one of the central communication stations. The preferred duty cycle over which the second communication signal is transmitted is about fifty percent of the second transceiver duty cycle. The communication system uses Time Division Multiplexed (TDM) communication signals using a number of channels as designated address channels (56) with the remainder (58) being used for data transfer.

Description

ALTERNATING SEQUENTIAL HALF DUPLEX COMMUNICATION SYSTEM
BACKGROUND OF THE INVENTION
Field of the Invention The present invention relates to communication systems and more particularly to two-way telecommunication systems employing central message transmitting stations and Earth orbit relay satellites to transfer messages between mobile terminals and the central stations. The invention further relates to a two-way telecommunication system using a sequential, alternating, half duplex communication pattern to reduce complexity and power requirements for each terminal while providing reliable communications between a large number of mobile system users.
Background of the Art
There is an ever increasing need for communication systems to provide message delivery or brief transfers of information between a central communication office or dispatcher and a number of remote system users. There are a substantial number of commercial, governmental, and private applications requiring the delivery of relatively short messages to or from a large number of geographically dispersed terminals, or mobile transceivers, often on an irregular basis. The need for message services includes such diverse applications as government services (military, law enforcement, legislative) where secure communications are desired, forestry, resource management, disaster relief or coordination, aviation, navigation, commercial transport or transportation, and message delivery services. Other examples include the interstate trucking industry where dispatchers wish to communicate short messages to trucks located anywhere in continental U.S., especially in rural areas. Presently the transfer of such messages is restricted to periodic telephonic communication between drivers and a central dispatcher or contact person. Currently, truck drivers must call long distance from many remote geographic locations to retrieve messages or to update delivery and pick-up schedules. However, it is hard, if not impossible, for drivers to consistently "call in" at fixed, scheduled, times since telephone services are not always readily available in many areas. The conventional "call in" approach also creates accounting problems and major personal inconvenience by requiring vehicle drivers to use money or charge cards for long distance calls at substantial cost even when no updated message or information is transferred.
Aside from conventional telephone systems, other communication systems have attempted to address the mobile market. Radio telephone, cellular telephone, and portable radio transceivers (CB) are all capable of providing some form of communication between a mobile transceiver and a base unit. However, these communication systems suffer from several drawbacks and have proven inadequate as message communication systems for serving a large number of widely dispersed users.
Current mobile communication services operate on a limited number of high frequency, low data rate, channels and have many more potential users than system capacity. Many systems, like cellular telephone, employ frequency reuεe across an array of cells to increase capacity, with each cell having a short transmission range to increase frequency reuse and reduce interference. However, these lower power transmissions are more prone to frequency selective fading and signal blocking and require highly mobile users to frequently change channels as new cells are traversed. These systems are also prone to sudden communication loss when no channels are available in adjacent cells. Cellular systems economically serve large metropolitan areas but leave many urban and most rural areas without any service or direct coverage at all. Messages for these areas are switched to conventional telephone or satellite carriers for long distance transfers to ground based systems which eliminates the flexibility desired. There ar no direct satellite communication systems.
Direct communication, non-cellular, using traditional mobile radio transceivers also requires constant monitoring of a variety of frequencies all of which are crowded with existing traffic. These services, like cellular telephone, are subject to frequent system overload and signal degradation from several interference sources which makes them incapable of handling a large volume of traffic. These transceivers also have a low range imposed by the need to prevent interference with other communication systems.
Communication systems based on Earth orbital relay satellites have been proposed as a new approach to solve many communication problems, especially coverage of geographically diverse, low user density or rural areas. Several systems have been proposed or developed to operate through orbital relay satellites and central communication stations. Examples of such systems are found in U. S. Patent Nos. 4,291,409 and 4,455,651.
However, the high gain, low interference requirements imposed on such systems, especially in regards to adjacent Earth orbit relay satellites or concurrent satellite users, requires the use of large, narrow-beam, receiver antennas on the order of 4 feet or more in diameter, which eliminates mobile applications. In addition, these satellite systems are limited to low data transfer rates which severely limits the number of potential users and data transfer capacity. Otherwise, tracking and demodulating a high data rate satellite signal requires very high speed, complex, and expensive, receivers that also consume a lot of power for signal scanning and processing even when not receiving messages. Such equipment is impractical for a commercial message system.
What is needed is a communication system that allows continuous delivery of messages and related communication parameters or control information to a large number of users over a large geographical area. The system needs to provide a return link for message acknowledgment and responses. A system that allows the development of a complete private digital data network. The system needs to be cost effective, simple to operate, maintain, and install, and minimize antenna requirements. The system should also automatically adjust to handle many transfer errors associated with a mobile environment. SUMMARY OF THE INVENTION
With the above problems of the art in mind it is a purpose of the present invention to provide a two-way message communication system capable of accommodating a large number of geographically diverse users.
An advantage of the present invention is that it provides a modulation scheme that provides performance comparable to a predetermined signal to interference ratio in any interference scenario encountered. Another purpose of the invention is to use a novel modulation, coding, and multiplexing technique which allows an inexpensive two-way mobile terminal with a very small antenna suitable for use on a moving vehicle, to receive and transmit data reliably using a satellite repeater. Yet another purpose of the invention is to provide a modulation and coding scheme that is implemented digitally, preferably as firmware in signal processing chips of the VLSI type and in microcomputers.
Another advantage of the present invention is that the communication signals can be more effectively screened from existing communication services.
Yet another advantage of the present invention is a high performance, cost effective, and flexible implementation. Still another advantage is that the present invention provides a modulation and coding scheme that allows mass production of circuits and modules to be used for the remaining analog functions for the mobile terminals.
An object of the invention is to allow flexibility in data transfer rates so that receivers of differing transfer rates or capabilities are efficiently accommodated in a single system.
A further advantage of the system that results from the latter object is that more energy per bit can be used to compensate for unequal downlink power density across large geographical areas.
These and other purposes, objects, and advantages are realized in a message communication system for sending messages between central communication stations and one or more mobile terminals through Earth orbital relay stations comprising at least one central communication station having a first transceiver for transmitting a first communication signal from the central station to one or more mobile terminals and at least one mobile terminal having a second transceiver for receiving the first communication signal and demodulating it, and for transmitting at a predetermined duty cycle for the second transceiver, a second communication signal to at least one of the central communication stations. The preferred predetermined duty cycle over which the second communication signal is transmitted is about fifty percent of the second transceiver duty cycle. At the frequencies of interest the fifty percent duty cycle is on the order of 10 - 20 milliseconds in length. In a preferred embodiment, the communication system first and second transceivers transmit and receive Time Division Multiplexed communication signals which comprise N serial channels, with D data channels (D < N) used for transmission of message data and A address channels (where A = N - D) used for transmission of address information. The address information is in the form of terminal addresses where messages are designated to be sent.
The central communication stations employ a terminal assignment device which determines which terminals in the system a message is directed to and, accordingly, assigns a terminal address to the message; and a channel assignment device for assigning each message to at least one of the data channels for transmission. An address controller transfers a terminal address and an associated data channel assignment onto one of the address channels in response to input messages intended for each terminal. Alternatively, where a message is intended for several terminals, multiple addresses are designated or assigned to a message. Also, special group or all call addresses can be associated with each receiver to facilitate multiple receiver addressing with a minimum of address information when possible.
A message input control device is connected to the channel assignment device and receives digital messages and transfers them serially onto designated data channels in response to an assignment from the channel assignment device at a rate of one message per channel at a time. The input message data is nominally transferred at a rate on the order of at least 5,000 bits per second.
In a preferred embodiment the communication system applies Golay [24,12] block coding to the digital messages prior to transmission and applies a corresponding Golay [24,12] block decoding process to resulting symbol data when received. The Golay coding generates digital symbol data at a rate on the order of 10,000 bits a second. In addition, a checksum computation is performed on input digital messages with a series of bits being added to the end of the message for checksum verification by the receiver.
In further aspects of the invention, the operating frequency of the TDM communication signal is frequency hopped at differing rates between the forward and return links over a preselected number of frequencies to decrease the power density of communication signals.
A unique triangular waveform is used to modulate the RF carrier center frequency with a 2 MHz peak to peak amplitude and a period of 30.24 milliseconds. This causes a triangle wave power dispersal so that the forward link has the same interference characteristics as a single video carrier saturating the transponder so that no unacceptable interference is generated for satellites adjacent to or within 2° from the satellite 20.
The central communication station uses an input or conversion element to convert incoming message information from digital or analog sources into digital messages at a predetermined transfer rate on the order of 5,000 bits a second. The digital messages are then used to modulate a carrier to form the desired communication signal. The transmitter is connected to at least one narrow-beam antenna which directs communication signals to a preselected relay satellite. The communication system of the present invention uses mobile terminals having small, portable, directable, narrow- beam antennas connected to a demultiplexer and other means for detecting, demodulating, and decoding the TDM communication signal so as to receive message data. The mobile terminals take advantage of the alternating duty cycle for transmission and reception to monitor the parameters of received signals and use changes as a guide to alter return link signal characteristics. In addition, the transceivers employ a single set of local oscillators for both transmit and receive functions.
BRIEF DESCRIPTION OF THE DRAWINGS
The novel features of the present invention may be better understood from the accompanying description when taken in conjunction with the accompanying drawings in which:
Figure 1 illustrates an overall diagram of a communication system operating according to the principles of the present invention; Figure 2 illustrates an overview of the message encoding/decoding and channel multiplexing of communication signals used in the system of Figure 1;
Figure 3 illustrates a schematic representation of exemplary circuit functions employed in a transceiver for the system of Figure l; and
Figure 4 illustrates a schematic representation of exemplary demodulator/modulator circuit functions employed in a transceiver for the system of Figure 1.
DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT
The present invention provides a method and apparatus for transferring messages between one or more remote, mobile terminals and a series of one or more central communication stations or Hubs. The communication system provides this information transfer for a large number of users by using a Ti e Division Multiplexed (TDM) communication signal having message transfer channels and receiver address channels which are used in an alternating half duplex mode. That is, forward link and return link transmissions or reception for the central communications stations as well as mobile terminals alternate between a send and receive mode on a predetermined periodic basis to allow use of common elements in the up and down conversion chains as well as in the IF elements to minimize complexity and costs. At the same time, this alternating communication scheme allows TDM mode tracking and error correction which improves communications.
An overview of a communication system operating according to the principles of the present invention is illustrated in Figure 1. In Figure 1, a communication system 10 is illustrated having a mobile terminal (not shown) mounted in a vehicle such as a truck 12. The truck 12 represents any of a variety of vehicles whose occupants desire to obtain occasional or updated information, status reports, or messages from a central communication source. As previously discussed, truck drivers or various drayage personnel often have a need for ready access to messages for more efficient operation.
It is also very desirable to have a mobile system user be able to communicate at least some form of limited message or acknowledgment to the central control station in response to received messages. A reply message may prevent the need for further communications or may indicate a need for an additional instruction or updated message from new information provided by a vehicle driver. At the same time, by providing for a return link of communication, even if limited in content, it is possible to incorporate other features into the communication link such as simple message acknowledgment to provide verification of message receipt by the terminal whether or not the driver operates on the information. Other automatic responses may also be configured into the operation of the transceiver such as location and vehicle status.
The return link allows a driver to enter messages such as a verification of time and delivery information, or a report on current position or other status information.
A message is transmitted to the truck 12 from a central transmission facility or terminal 14 referred to as a Hub facility. The central terminal or Hub 14 can be placed at a location such as a trucking terminal or central dispatch office allowing lower cite costs and local, direct, access to transmission equipment for maintenance and system upgrade.
Alternatively, the Hub 14 is located in a remote location more ideally suited for low interference ground-to- satellite transmission or reception. In this case, one or more system user facilities in the form of central dispatch offices, message centers, or communication offices 16 are tied through a telephonic, optical, satellite, or other dedicated communication link to the Hub 14. In addition, for large numbers of remote customer message centers, a message or network management center 18 can be employed to more efficiently control the priority, access, accounting, and transfer characteristics of message data.
The Hub 14 or management center 18 can be interfaced to existing communication systems using well known interface equipment such as high speed modems or codecs which feed message signals into the communication system 10. High speed data management computers can also be used to determine message priorities, authorization, length, type, accounting details, and otherwise control access to the communication system 10.
The Hub 14 employs an Extremely High Frequency (EHF) transceiver to establish an forward and return link or up and down link communication paths with a geosynchronous Earth orbiting relay or repeater satellite 20. These links are maintained at one or more of a number of preselected frequencies or frequency ranges. A typical satellite system employs a series of repeater transponders for transmitting 12 GHz frequency signals for TV or radio transmissions to ground stations.
The preferred embodiment of the communication system 10 employs uplink and downlink carrier frequencies in the EHF Ku band to allow access through the transponders on existing or new communication satellites already launched or planned. The communication system 10 can take advantage of unused or excess satellite capacity at these frequencies and does not require the launching of its own, new, dedicated satellites. Therefore, the benefits of the present invention are immediately available without additional expensive satellite technology. However, the communication system 10 can also be implemented at other frequencies dependent upon available satellite transponders and can provide improved communication through some ground based repeaters.
The Hub's transmission signal is transferred through a diplexer 22 to an antenna 26. The antenna 26 comprises a very small aperture antenna for directing the communication signal 24 to a single orbiting satellite.
A forward link communication signal, designated 24a, is transmitted through the antenna 26 to the communications satellite 20 at the preselected uplink carrier frequency. The communication signal 24a is received.by the repeater satellite 20 where it may be translated to a second frequency for the downlink transmission 24b. Those skilled in the art of communications understand the apparatus needed to perform this reception and conversion function which are known in the art. Using different frequencies for the uplink and downlink communication signals reduces interference.
Current satellites typically support a number of independent communication channels with about 48 Mhz of bandwidth. These satellites use polarization isolation to obtain frequency reuse, with one set of channels operating at one polarization (horizontal or vertical) and another set operating at the same frequency with an offset of 1/2 channel and operating with a 90° polarization shift. This 90" polarization shift is normally applied between forward link and return link communications for one communication channel with one transponder used for the uplink and one for the downlink.
The transmitted forward downlink signal 24b is received by a mobile transceiver 70 (Fig. 4) through a small, generally directional antenna 30. The antenna 30 is constructed to have about 15 dB of gain and to be directional within a 40-50° elevation beamwidth and 6-10" azimuthal or orbital arc beamwidth. The antenna 30 is mounted so that it is capable of being continuously rotated over a 360 degree arc and has an unobstructed filed of view for the satellite 20. The antenna is connected to an antenna pointing and tracking control system 74 (Fig. 4) for tracking the satellite 20 as the vehicle 12 changes position relative to the satellite. An exemplary antenna rotation mechanism is found in co-pending U. S. Patent Application
SN. , , and an exemplary method of satellite tracking is disclosed in co-pending U. S. Patent Application SN. , both of which are assigned to the assignee of the present invention.
Messages, or message data, are transferred into the Hub 14, or control station 18, where they are converted into digital message signals which at a rate on the order of 5,000 bits per second. Those skilled in the art will readily understand that the teachings of the present invention apply to higher, or lower, data transfer rates when circuitry operating at the appropriate speed is employed. Messages can be received directly as digital data at various bit rates and accumulated or stored for translation to the desired system transfer rate. Alternately, messages are received as audio message signals that are keyed in by system operators to form the desired message signals. In addition, some message information is generated internally or directly by the network management center 18 for communicating system type data, such as time, terminal assignments, rates, etc.
Each message signal can be subjected to a variety of coding, encryption, or error detection and correction schemes prior to transmission. Where desired, individual terminals can employ unique codes or ciphers to provide secure message delivery capabilities. However, to reduce transmission errors and provide for error correction for all messages transmitted by the communication system 10, at least two encoding steps are implemented for all digital messages or message data.
One step comprises applying a system 10 checksum algorithm to the digital message data. In the preferred embodiment, the checksum algorithm employs on the order of 30 bits of information to indicate the values resulting from checksum computations which are used to detect transfer errors. An exemplary checksum formula for use in the communication system 10 is the computation of the polynomial: X30 + X29+ X3+ X2+ X + 1. When calculating this checksum the address field (see below) of a message is ignored so that channel addresses do not alter checksum values.
A second step comprises encoding all data, message, instructions, or addresses, using a Golay [24,12] block code to encode every 12 bit block of information, including checksum, type and recipient information, into 24 binary symbols for transmission. These 24 bits are then transferred at the desired system transfer rate. Using the Golay [24,12] block coding scheme means that 5,000 bits of message data forms a 10,000 bit encoded symbol stream for transmission. Therefore, the system 10 transmission signal rate is about 10,000 binary symbols or bits per second to accommodate the 5,000 bit per second input data rate. On the reception end, the code symbols or blocks are decoded to regenerate the 12 bit blocks of information. As known in the art, the operation of a Golay [24,12] or similar code acts to minimize transmission error by decreasing the impact of single bit errors on a data stream through spreading the data out over multi-bit patterns. Each bit error affects only a fraction of a bit in the message which is effectively compensated for by the error correction schemes used until very high error rates occur.
The encoded message symbols are used to modulate a frequency generator or source such as a Direct Digital Synthesizer which creates an FM modulated carrier, at a preselected frequency which is up-converted to the desired EHF band for transmission to the satellite 20. The encoded symbols can be used to drive a BPSK modulator which is coupled to the carrier wave source for the communication system 10. In the preferred embodiment, each symbol is shifted in phase from the previous symbol, either -90" to indicate a 0 or +90° to specify a 1. This is referred to as Differential Advance Retard Keying and improves acquisition by the terminal because every symbol contains a phase transition. To decrease interference and accommodate a large number of terminals at potentially different burst rates, a Time Division Multiplexed (TDM) transmission scheme is used. The TDM approach divides the total transmitted (or received) spectrum into temporal increments or frames of predetermined length. Messages or message signals transmitted in or by the communications system 10 are allocated portions of this time controlled sequence known as channels, and no other signal uses the system at exactly the same time. The allocated portions or channels are very small, temporally, and their interleaving across successive frames very large so that communication appears simultaneous to all terminals. Methods and apparatus for generating, transmitting, and controlling TDM signals are well known in the communication art and can be accomplished using a variety of signal multiplexing and control devices.
Each frame consists of a number of channels which represent substantially identical, sub-frame length periods during which symbols are transferred. This means that messages or message signals are transferred a few bits at a time during each successive frame until the message is completed. The preferred embodiment divides each frame into 25 sub-frames or channels. However, those skilled in the art will readily understand that the number of channels depends on the transmitting speed of the communication system 10, number of users to be accommodated, and frequency hopping schemes as described below.
In using the TDM approach, information is generally sent over the communication signals 24a, 24b in discrete packets. The communication system can accommodate packets of differing lengths between 4 to 256 characters each, depending on the type, burst rate, or size of messages being transferred. In addition, the messages, preformatted or free-form, are generally limited to 2000 characters in length to facilitate transfer speed and high message capacity.
Each packet is generally segmented into fields of information such as the type of message, typically a 6 bit entry to distinguish between possible alternative system formats, the length of the message, to allow proper tracking, the body of the message, and the checksum bits. There is also an address field of 24 bits associated with each message as discussed further below. Those skilled in the art will readily understand that some "zero packing" will be used from time to time to assure a uniform frame size regardless of overlapping message lengths, varying packet sizes and transmission rates, or empty channels. However, unused channels generally will have random data transmitted to improve tracking and acquisition of channels by transceivers. To assure that each transceiver is tracking and demodulating a designated channel, a series of codes or code masks can be used with the data to detect tracking errors. That is, short bit patterns can be added to the data transferred by each channel to allow automatic differentiation from data in adjacent channels. Once a transceiver commences demodulating one channel it records the code mask for that channel. The mask is used to decode or demodulate all data received until the end of the message. If the transceiver erroneously uses data from adjacent channels, the code mask will prevent incorporation into the message.
In order to further reduce interference by increasing isolation and, thereby, increase the system 10 message capacity, Frequency Hopping (FH) of the carrier frequency can be used. An FH technique spreads the power density of the signal 24 over the entire transponder 48 MHz bandwidth, reducing downlink power density which minimizes interference with other communication services and provides processing gain which the transceivers use in rejecting the interference of other services. The basic techniques of FH- TDM transmissions are known in the communication art and also provide a vehicle for spreading a signal out over a given bandwidth so that transmission errors caused by frequency selective fading or other aberrations only affect a small portion of the signal. At the same time, frequency hopping according to a unique pattern allows some degree of security for some system 10 users.
In the preferred embodiment, the forward link FH scheme comprises dividing the appropriate forward link (downlink) transponder bandwidth (11.7 - 12.2 Ghz) into 240 frequencies located approximately 2.5 MHz apart. The hopping rate for the frequencies of interest is on the order of 200 frequencies per second covering the 240 discrete hopping frequencies before recycling. This means that the dwell time for each frequency is about 5 milliseconds. If each TDM frame is transmitted at a new frequency then each frame is about 5 milliseconds long and the size of each channel is roughly 0.20 milliseconds in length.
The frequency hop pattern can comprise a simple linear progression from high to low or vice versa, but a more complex pattern based on a pseudo-randomly generated frequency selection sequence is preferred. However, those skilled in the art will also recognize that a TDM signal without frequency hopping will benefit greatly from the method and apparatus of the present invention.
Returning to the desired transmission rate of 10,000 symbols per second or 1 symbol every 0.10 millisecond, it is seen that each frame period allows 2 symbols to be transmitted per channel. This would imply a transmission rate of forty-eight (48) code symbols every frame. However, to improve reception, the preferred embodiment uses a fifty (50) symbol transmission rate for each frame with the first symbol period employed for settling time to assure that the transceiver has locked onto, and the transmitter is accurately within, the selected frequency and not offset due to the changing characteristics of the frequency source.
The second symbol is used as a phase reference for the third symbol in the stream of fifty symbols, with the third symbol being the first message symbol. Each successive symbol is used as a phase reference for the next. This relies on a differentially coherent demodulation scheme as opposed to an absolute phase reference since absolute reference approaches are more complicated and extremely difficult to achieve in a mobile communication system. The code blocks or symbols are divided into alternating groups or sequences. That is, every other code block is selected and placed in one 24 symbol group for transmission. This separates every other code symbol from its adjacent symbol which spreads code symbols that are close together in code to be far apart in time. This interleaves the code blocks to provide a means of minimizing signal errors generated as a burst of errors in a sequence by spreading the message signal over a wide signal bandwidth.
The FH-TDM type communication signal 24a is transmitted by the Hub 14 through the repeater satellite 20 (where it becomes signal 24b) to all of the terminals within a given geographical zone or region serviced by the satellite. This zone can be as large as an entire country, or as narrow as a small state depending on the application. However, regardless of the zone covered by the satellite, each ter inal in that zone normally would have to detect, monitor, and demodulate the signal 24b in order to receive messages. If the messages are simply applied across all of the channels, then each transceiver has to continuously track, demodulate, and decode the entire wide bandwidth signal to assure reception of a relevant message. This would be required because every message header or lead-in in every channel would have to be scanned by each transceiver to verify which terminal is designated to receive the message. For large numbers of users this requires very high speed, complex, demodulation circuitry to accomplish. Since speed and complexity increase system cost and decrease reliability, this is undesirable.
In the present invention, terminal selection is accomplished using a new terminal or transceiver addressing technique for TDM communication signals which comprises a two part addressing scheme. This technique is explained in greater detail in copending U. S. Patent Application SN.
, also assigned to the assignee of the present invention.
In this technique, each terminal is assigned a unique system address which is known to all Hub 14 transmitters or system management centers 18 used by the communication system 10. The terminal address establishes an individual identity for each terminal in the system. This address is generally set at the time of terminal manufacture or installation and can be made unalterable by a transceiver user or made dynamically changeable by the system 10 depending upon the system requirements or costs. In the preferred embodiment, the transceiver addresses are designated or determined by a 19 bit address term making approximately 524,288 (2 19) terminal addresses available which allows a very large number of users for the message communication system 10. In addition to the "individual" address, terminals can also respond to specialized "system" addresses such as a
"group" address (if applicable) , an "all-call" address, or other "conditional" addresses. By providing these alternate addresses to which a terminal, can respond, it is possible to very efficiently transfer single messages to an entire system or a group of terminals without sending the same message to every designated transceiver over a longer transmission period. This also provides for the transmission of system type information such as time of day, service changes, etc. , to all terminals on a periodic basis, by interleaving these types of messages into otherwise unused channel capacity.
With terminal addresses defined, the communication channels in the FH-TDM communication signals 24 and 28 are divided into an address portion of A channels and a data or message portion of D=N-A channels. In the preferred embodiment A is 4 and D is 21. However, other values for the total number of channels and address channels can be used depending upon specific system requirements. The A address channels are used to transmit address information and designations for those terminals whose messages are being transmitted by the Hub 14. The D data channels are used to transmit the messages for the designated terminals. The transmission of each message address precedes the transmission of that message by a predetermined period of time to allow a terminal to adjust its, tracking circuitry and synchronize with the appropriate channel before the arrival of the message.
The address channels are typically designated as system channels 1, 2, 3, ... etc. However, these channels can be separated by data channels where channel tracking either permits or desires this spacing for transceiver demodulation. In addition, the number of channels can be dynamically adjusted by the system 10 to accommodate several problem situations. One problem arises when there are a great number of messages, saturating the address channels but the messages are short, thus leaving excess data channel capacity. In this situation, a data channel could be reassigned to be an address channel. The opposite problem occurs when there are an average number of messages but they are all maximum length. The system 10 may find it advantageous to use one of the address channels for data to decrease the number of messages being backlogged.
This addressing scheme means that address information only needs to be demodulated at a fraction of the communication signal rate allowing each transceiver to monitor the communication signal 28 at this lower rate until it detects its address. When a terminal detects its address, accompanied by a channel assignment, the transceiver switches to the appropriate channel and begins demodulating and receiving the message. Therefore, it will be apparent to those skilled in the art that transceivers are not demodulating nor decoding the entire, or even a majority of the communication signals 28 transmitted by the communication system 10. This allows a less complex and slower speed reception circuit which reduces power and cost while increasing reliability and ease of construction. Where desired, each transceiver can be assigned a specific address channel to monitor, dynamically or fixed, which further reduces processing to a 1/N rate for both addressing and message demodulation.
Reception and decoding of communication signals is illustrated in further detail in Figure 2. In Figure 2, an incoming communication signal comprising interleaved code symbols 50 is received by each transceiver on a series of signal channels 52 which are frequency hopped in a sequence of hops 54. The messages are received on the data channels 56 while address information is received on the address channels 58. The digital code symbols comprise the code block symbols described above and are received at a rate of two symbols per channel per frequency hop. There are two extra symbols received during each hop with the first disregarded or lost due to settling of the transceiver and the second being used to obtain the phase required to track the third symbol. Therefore, there are forty-eight information symbols per frame in each hop and 48 symbols received for each channel after 24 hops.
After 48 symbols are accumulated they are sorted into a first and second series of symbols shown in Figure 3 as "A" symbols and "B" symbols with each group having 24 symbols. Both message and address code symbols are sorted into 24 symbol code blocks 60 using a sorting step and apparatus. This process removes the interleaving previously impressed on the code symbols as they were transmitted. As can be readily understood by those skilled in the art, those symbols that were close in code are transmitted far apart in time which provides isolation from errors as previously discussed. Every block of 24 symbols, "A" or "B" is decoded into successive 12 bit blocks 62 using a Golay. [24 , 12] decoder. The Golay [24,12] decoding step yields 12 bit blocks of transmitted data. This data will be generated or received at about 5,000 bits per second as originally transmitted (before encoding) . The 12 bit blocks of information now comprise a series of address assignments or messages depending on which channel they were received on.
The output of the address channels 56 comprises 24 bit length information sequences 64 which use 19 bits to specify a transceiver address within the communication system 10 and 5 bits to indicate a channel selection for receiving a message directed to that transceiver. Each message has an address 24 bit segment associated with it which is segregated from the message and transferred over the address channels to flag an appropriate transceiver.
The output of the message or data channels 58 comprises a series of successive 12 bit blocks 68 which comprise a header that indicates the type of message, including its length, a main body of the message and a series of checksum bits for error detection. The length of the incoming message is important so that the transceiver can properly track the entire message or provide an indication of error if the entire message is not received.
As previously discussed, it is clearly understood that address information for a transceiver is sent before the message is transmitted on a data channel. The amount of "lead time" for transmitting address information depends on the channel switching speed of the transceivers as would be known by those skilled in the art. The address must be provided prior to the message by a time period equal to this switching time plus some settling time for the transceiver to properly and accurately track the designated channel.
An exemplary transceiver for receiving the communication signals and providing a message output is illustrated in schematic form in Figure 3. In Figure 3, a transceiver 70 is shown for receiving and demodulating communication signals from the Hub 14 and satellite 20. The transceiver 70 is connected to the antenna 30 through a diplexer 32 for receiving the satellite downlink signal 24b which is transferred into a demodulator 72 for demodulation into an encoded symbol stream (digital message) .
The demodulator 72 employs elements known in the art for down-converting the received communication signal 28 to a lower IF frequency level and then symbol frequency level (10K symbol bits per second) . A local oscillator and other reference signal sources would be provided for mixing with the communication signal 24b along with one or more bandpass filters. Once the signal 24b is demodulated and decoded it is transferred to memory storage for accumulation of a message and other processing steps. The demodulator 72 transfer rate is synchronized with the modulator used in the Hub 14 or the satellite 20.
Synchronization for the transceiver 70 is accomplished by tracking and synchronizing with the frequency hopping pattern of the communication signals. Once a transceiver haε synchronized with the frequency hopping of the TDM signal frames then the internal frame timing is automatically detected as well. The mobile transceiver or terminal 70 incorporates a low cost microprocessor or similar controller 74 for implementing signal processing, acquisition, and demodulation functions. A low noise amplifier 76 and the conventional down-conversion chain of the demodulator 72, provide a signal to the microprocessor for signal acquisition, tracking and demodulation. Information from the demodulator 72 or the microprocessor 74 is provided to an antenna tracking and pointing controller 78.
The antenna 30 is generally swept through a series of 360" arcs by the controller 78, until a signal is detected from the satellite 20, in the receiver's frequency range, above a predetermined threshold. At this juncture one or more tracking and signal processing algorithms are used to determine the direction of highest signal strength and the antenna tracks that direction relative to receiver or vehicle 12 position or movement.
Many of the individual functions performed by or under control of the microprocessor 72 are illustrated as separate elements in Figure 4 for purposes of clarity. However, those skilled in the art will readily appreciate that the functions surrounded by the dashed line 75 can be performed in a single miniaturized circuit by an integrated circuit microprocessor and related support chips. This allows implementation in a high reliability, low cost, low power consumption circuit or using VSLI technology. A receiver address storage element 82 is connected to the demodulator 72 for storing the address assigned to the receiver 70 and used to determine the presence of a message from the satellite 20 or Hub 14. The address storage element 82 typically comprises a small ROM or similar memory device connected to the microprocessor 74. The address can be hardwired into the microprocessor structure itself such as in the case of scratch memory, or internal RAM although this may not be convenient or cost effective in many applications. In addition, the use of a separate memory element allows alteration by service personnel at a future time where needed.
It is also possible to store the receiver address on a portable storage element such as a magnetic strip or cartridge which can be read by a card reader (not shown) connected to the microprocessor 74. This would allow individual communications system 10 users to move between receivers which are permanently installed in a variety of vehicles and automatically receive messages without informing a central dispatcher of a new receiver location.
Once a receiver address matching that stored in the address storage 82 is detected, the channel designated by the corresponding address information is also received and registered by the receiver 70. The receiver 70 automatically switches to synchronize reception on that channel and begins demodulating a message signal.
If the antenna fails to track the communication signal 28 at any time during the reception of a message, or any type of signal failure or blockage occurs, one or more errors will be detected in signal demodulation and no message will be displayed. Such errors would could include premature termination of the message before the length, time, specified in the message header or the failure of the checksum verification process. The demodulated communication signal is transferred to a decoder 80 where Golay decoding occurs. At the same time, a pseudo-random code source or other related code storage element 84 provides any necessary code sequences required to further decode a received message. The decoded message bits may be temporarily stored in a memory element 86 before visually being displayed by a display element 88. An exemplary display element comprises a two to four row, twenty to eighty character wide display unit capable of running from relatively low current. The individual segments of the display can comprise LED, LCD, electroluminescent, or discharge element type character displays. Consideration must be given to the brightness generally required in a vehicle environment to prevent undue distraction of a drivers attention. The display unit 88 should be as compact and lightweight as possible so that it can be mounted in an easily viewed location. In addition, the display can incorporate a message ready indicator or message error indicator so that the receiver users knows that a message was sent.
Alternatively, the message can be interfaced to other processing elements, such as a portable computer, through an interface device or connector 92 or printed out by a hard copy device 90, such as a small thermal printer. What has been described to this point is the forward link which provides the advantage of delivering messages to a large number of users in almost any location, metropolitan or rural, throughout the country with high reliability and relatively low cost.
However, the communication system 10 offers the added advantage of a return communication link so that short responses can be made to received messages where desired.
For the return link each transceiver or mobile terminal uses a low power signal on the order of 1 Watt and an antenna gain of about 19 dBi for a transmit power of 19dBW. The return link is transmitted at a higher frequency than the forward link to decrease interference. The frequency chosen is in the typical satellite Ku band transponder range between 14-14.5 GHz. However, as before other frequencies can be employed for this return link.
The return link communications signal 28 uses a FH waveform similar to the forward link but takes advantage of typically slower data transfer rates occurring from a mobile communications terminal. That is, return messages or data are not going to be entered into a local terminal at high speeds where a terminal operator is manually responding to a message. Where acknowledge and other prestored signals are used they are adjusted to a slower bit rate to comport with the slower manual entry mode.
Since data is typically provided on the return link at slower rates on the order of 100-140 bps maximum, and more typically 22-48 bps, the FH rate needs to be decreased on the return link in order to allow sufficient dwell time for each channel to transmit the data. To transfer Golay [24,12] encoded data this becomes 280 symbols per second. Therefore, the forward link rate of 200 frequencies per second should be reduced to about 60 frequencies per second. Messages being input to the transceiver 70 are subjected to a rate 1/3, k=9 forward error encoding convolutional code.
The small, portable and directable antenna 30 typically has a beamwidth on the order of 6-10' , which is wide enough to encounter more than one satellite. Therefore, steps are taken to provide a return link waveform that does not interfere with existing services on adjacent satellites.
A direct sequence spread spectrum coding function is applied to the return transmission to spread the signal out over the transponder bandwidth and make the communication signal 28 appear as relative noise to adjacent services. For this application a short direct sequence pseudo-random code is used. This code is typically applied to a direct digital synthesizer or similar modulated frequency driver. In the alternative, or in addition, either the forward or return link communication signals are modified by modulation with a special modulation waveform that disguises the signal to other services.
All satellite communication services currently configured to detect and prevent interference by standard video data or signals since a majority of satellite usage is for television and video type broadcast transfers. Therefore, all satellite services, video or otherwise, must be able to detect and isolate video signals which are transmitted employing a triangular wave form of modulation. In the present invention, this general waveform is mimiced so that other systems perceive communication signals 24 or 28 as video signals which are ignored. This is accomplished by modulating the RF carrier center frequency for the Hubs 14 or transceivers 70 with a triangular waveform having a 2 MHz peak to peak amplitude and a period of 30.24 milliseconds. This causes a triangle wave power dispersal so that the forward link has the same interference characteristics as a single video carrier saturating the transponder so that no unacceptable interference is generated for satellites adjacent to or within 2° from the satellite 20. The triangular modulation can be implemented by altering the characteristics of a DDS output which will accurately track a triangle wave and yet transfer more information than a true video signal. To facilitate frequency coordination, the center frequency is fully synthesized at the Hub and mobile terminals and can be placed anywhere within the transponder, after informing the transceivers of the new center frequency. hile interference by the transceiver 70 with other services has been discussed, this is not the only restriction on optimum operation. The transceivers 70 must also be able to quickly and reliably acquire the Hub 14 or satellite 20 transmissions and continue to track them while moving. In addition to interference from other systems, the transceivers 70 face interference and loss of signal due to a variety of inherent impediments for mobile communications, including doppler effects, frequency fading, etc.
The present invention counters many of these problems by assuming that there may be significant changes in the transmission capability of the communication system 10 on a very short time scale, interpreting any change to altered environmental conditions, and adjusting for such changes. Each transceiver 10 monitors the quality of or results of communication with the Hub 14 and periodically adjusts operational parameters to maintain or improve communication links accordingly.
This is implemented in the present invention by operating all transceivers in an alternating half-duplex transmission/receive scheme. Transceivers are operated in a half-duplex mode with transmissions done at a 50 percent duty cycle to allow for continued antenna tracking and error correction based on received downlink signals.
If at any time the downlink signal is lost then transmission also terminates to assure that unacceptable interference is not generated.
If the signal is lost, as previosuly stated, any partial message is deleted from memory and not present for display. However, another key criteria is that if there is no downlink then the transceiver uses this information to recognize that there is no uplink. Actually an uplink may be possible and the error could be in the receiver only. However, the system assumes that without a downlink the uplink information is either not being received or is no longer needed. In any case, the transmitter function is terminated if the receiver link is terminated for any reason.
This provides a very good safety feature for commercial applications of the transceiver 70. If the reception were to be interrupted for any reason, including a person interfering with reception by stepping in front of or otherwise traversing the antenna path, then within a fraction of a second all transmissions from the antenna are terminated. Therefore, no radiation damage of any significance nor hazardous exposure can ever occur for the transceiver of the present invention making it ideal for broad distribution in a commercial (mobile) communication system.
The transceiver 70 is normally configured to be in a receive mode wherein it monitors an assumed satellite position or general horizon looking for a signal for incoming communications signals. This initial signal acquisition occupies the full duty cycle of the transceiver. Once a signal is detected, tracked, and acquired, the transceiver operates on the 50 percent duty cycle. Each half cycle is a very short period of time on the order of 15 milliseconds.
After signal acquisition, the transceiver 70 synchronizes with the forward link FH pattern and rate and switches to the correct channel frequency for receiving either channel address or a message. Then, every 15 milliseconds the transceiver 70 switches to the return link FH rate and pattern and for 15 milliseconds. However, the transceiver does not transmit until or unless requested to do so by the Hub 14 or communications management center 18. This assures that the Hub is prepared to receive the message and that there are no higher priority tasks in progress, including receipt of high priority emergency messages or alternate system 10 operating data. Also, polling controls the number and frequency of receivers to regulate interference at all times. The transceiver 70 then returns to the receive mode and continues to demodulate and decode the message, if any, so forth.
This alteration between send and receive on a periodic and short term basis provides the transceiver 70 with several operational advantages.
First, the transceiver monitors the power level .and characteristics of received signals every 15 milliseconds and detects substantial changes. The hub and mobile transceiver must agree well enough in terms of frequency to allow the transceiver to acquire and track the forward link signal. The transceiver will search +/- 18KHz about the nominal specified frequency
There are several possible sources of error. The hub 14, satellite 20, management center 18, and transceiver 70 all have internal reference oscillators for establishing transmission frequencies employed. Each of these references can drift and cause frequency errors. The satellite cause small frequency errors during translation of the communicaiton signals between up and down link frequencies. The transceiver 70 reference oscillator may drift and is subject to temperature change induced variations.
In the communication system 10 the Hub employs a Forward Link Processor (FLP) which adjusts transmission frequencies to correct for some of the possible errors listed above. First, however, the error in the Hub reference oscillator is assumed to be too small to measure. This is generally justified due to the fixed nature of the Hub facility and the heavily controlled environment and periodic maintenance such a facility undergoes.
Satellite translation error is measured and corrected by using a reference receiver at the Hub and using a testing or control pattern of information between the Hub and the reference receiver through the satellite. The FLP sends commonads to the satellite to adjust the translation frequencies to match what the Hub transmits. Any residual error, say from the control signals, is also assumed to be too inimaal to have an impact on communication quality. The transceiver oscillator drift is corrected by the transceiver according to a long term software program that assumes certain drift characteristics for the transceiver oscillator. Therefore, temperature drift is the largest reference error and it is corrected by comparison to the other references using the communication signals.
With the reference sources adjusted, the transceiver assumes initial frequency variations in singals are due to initial frequency tracking and synchronization mis¬ alignment. However, once a signal is acquired the receiver assumes that all variations are due to receiver positioning relative to the relay satellite or similar non-internal frequency problems. Therefore, the receiver assumes that antenna pointing and tracking must be adjusted when the overall power level of a signal decreases (as when a corner is turned) and that variations in frequency tracking are caused by doppler effects which must be countered. That is, variations in received frequency are assumed to be caused by changing characteristics of the communication link itself and not the error sources discussed above, which have been corrected. This means that errors in tracking frequency are attributed to Doppler shifts from vehicle travel and the frequency of both the receive and transmit functions of the transceiver are adjusted to accommodate this shift. Since the signal is constantly monitored on a short term basis, the present invention provides improved tracking and Doppler compensation.
Another advantage of the alternating half-duplex technique is that the transceiver does not need a full compliment of circuitry to handle both functions. That is, several circuit elements can be shared between the two functions since they are separated in time. Elements such as the antenna, antenna and related circuit feed cables, certain bandpass filters, and the transceiver local oscillators can be shared between the transmit and receive functions if configured appropriately.
In the present invention the transmit and receive frequencies are chosen to be within the preferred Ku or 11.5 to 14 GHz bandwidth as disclosed above. However, to achieve these extra high frequencies, one or more up-conversion stages or IF mixing stages are required in the transceiver 70 circuitry. It has been found that a series of desirable uplink and downlink or forward and return link frequencies within the specified bandwidth and FH scheme can be chosen so that they are separated by a very narrow margin in the intermediate IF stages and a common tunable local oscillator can be employed for both the transmit and receive function.
The result is that fewer components are required which reduces cost, increases speed and reliability (switching speed) and very importantly, decreases power consumption and size of the transceiver. A schematic diagram of a transceiver 70 analog modulation/demodulation section 100 operating according to the principles of the present invention is illustrated in Figure 4. In Figure 4, a modulator 100 is shown having a Fine frequency synthesizer 102 and a Coarse frequency synthesizer 104.
The coarse frequency synthesizer or Local Oscillator (L.O.) 104 represents a source of high to extra high frequency signals which is generally tunable over a broad range of interest in large steps on the order of 2-5 MHz each. An exemplary coarse oscillator for use in the present invention is a Phase Locked Loop (PLL) type oscillator generating output signals at frequencies on the order of 652 - 1175 MHz. in Steps Of 2.5 MHz. (652.5, 655, 657.5,...) The fine frequency synthesizer or oscillator 102 provides a finely tunable source of frequency with very low noise and is tunable over a smaller frequency range and or in smaller discrete steps. The fine frequency synthesizer 102 can comprise one of several frequency sources that provide a high accuracy, high resolution output in the frequency range between 5 to 20 MHz with direct digital synthesizers being preferred. An exemplary circuit for an advanced digital synthesizer useful in the present invention is disclosed in U. S. Patent Application SN. , filed January , 1988 and assigned to the same assignee as the present application.
In Figure 4 a single reference frequency source 106 is shown for use with the PLL of the coarse synthesizer 104, the fine synthesizer 102, other elements in the modulator/demodulator 100 and other oscillator and processing stages for the transceiver 70. This provides a system wide, synchronized reference or clock source which improves signal to noise ratio and allows simplified system wide synchronization with other system where desired. An exemplary reference source 106 provides a reference signal at 10 MHz from a highly stable reference source such as a rubidium standard.
Communication signals received from the hub 14 are received on the antenna 30 and transferred through an up/down converter 108 and through a band pass filter liυ to a power splitter 112. The power splitter 112 exhibits a 3db separation and is used to redirect received signals along a different internal processing path from the transmit signals and transfer them to a demodulation portion of the transceiver 70.
Incoming or received communication signals 24b are first mixed with the output of the coarse synthesizer 104 to down convert them to a lower IF freguency in the range of 250 + 7 MHz. This is accomplished using a signal mixer 114 which uses the communication signal as one input and the output of the coarse synthesizer 104 as a second input. The output of the mixer 114 is filtered by a band pass filter 116 to remove unwanted frequency components added to the down-converted communication signal by the mixer 114. The output of the band pass filter 116 is transferred to a second mixer 118 which has the output of the fine synthesizer 102 as one input. The mixing of these two signals provides a final IF frequency signal in the 20 + 20 MHz range. The output of the mixer 118 is transferred though a crystal filter 120 to the microprocessor 74 and subsequently decoded and displayed as a message for the transceiver 70.
When a transceiver 70 user has input a message through the display unit 88 or similar input means it is encoded and transferred into the modulator/demodulator 100 by modulating the input of the fine synthesizer 102. This is easily accomplished using direct digital synthesizer technology as understood by those skilled in the art. The output of the fine synthesizer 102 is applied to one input of a mixer 124 and the output of the coarse synthesizer 104 is applied to a second input of the mixer 124 to generate an intermediate IF frequency. This generates an output frequency from the mixer 124 on the order of 900- 1400 MHz when the coarse synthesizer 104 generates a frequency on the order of 652-1175 MHz and the fine synthesizer 102 generates an output in the range of 247 + 7 MHz.
The resulting transmit carrier, complete with modulated message data, is transferred to the up/down converter 108 connected to the transceiver antenna 30. The bandpass filter 104 filters unwanted frequency components from the transmit communication signal as it is transferred through the splitter 112 to the up/down converter 108.
The bandpass filter 110 is generally a single section varacter tuned voltage controlled type filter which removes local oscillator or synthesizer frequencies and low frequency images and also allows tuning to other frequency bands for use in the forward link demodulation.
The communication signal is up converted by the converter 108 to the desired 11.7 - 12.2 GHz range by mixing with 13.1 GHz reference. The up/down converter 108 can be configured as an output channel having a power amplifier connected to a diplexer for the antenna 30 with a mixer 130 connected to a local oscillator providing the 13.1 GHz mixing reference frequency. On the return link the up/down converter 108 presents a second mixer connected to the 13.1 GHz local oscillator for down converting received communication signals.
What has been described, then is a new method and apparatus for transferring messages between central communication stations and one or more remote, mobile, transceivers which allows low cost mass production of terminal equipment which achieves a high performance level in a variety of interference environments. The foregoing description of preferred embodiments has been presented for purposes of illustration and description. It is not intended to be exhaustive nor to limit the invention to the precise form disclosed, and many modifications and variations are possible in ight of thp above teaching. The embodiments were chosen and described to best explain the principles of the invention and its practical application to thereby enable others skilled in the art to best utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims and their equivalents.

Claims

1. A communication system for transferring messages between central communication stations and one or more of a plurality of mobile terminals through Earth orbital relay satellites, comprising: at least one central communication station having first transceiver means for transmitting a first communication signal? and at least one mobile terminal having second transceiver means for receiving said first communication signal and demodulating said signal, and for transmitting at a predetermined transmit and receive duty cycle, second communication signals to at least one of said central communication stations.
2. The communication system of Claim 1 wherein said predetermined duty cycle for said second transceiver means comprises a fifty percent duty cycle.
3. The communication system of Claim 2 wherein said fifty percent duty cycle comprises a period on the order of
10-20 milliseconds.
4. The communication system of Claim 1 wherein said at least one central communication station first transceiver means transmits and receives Time Division Multiplexed communication signals which comprise a series of N channels which are separated into A address channels and D data channels.
5. The system of Claim 4 wherein said central communication station further comprises: receiver assignment means for detecting which of said plurality of terminals each message is directed to; channel assignment means for assigning at least one channel to each of said messages at a time from said D channels; address control means for transferring a terminal address and an associated channel assignment onto one of said A channels in response to input messages intended for a terminal; and message input means connected to said channel assignment means for receiving digital messages and transferring said messages onto said D channels in response to an assignment from said channel assignment means at a rate of one message per channel.
6. The system of Claim 5 wherein said central communication station further comprises: at least one narrow beam antenna? and conversion means for converting information to be transmitted to a terminal into digital messages at a predetermined transfer rate.
7. The system of Claim 1 where in said second transceiver means has a demodulator/modulator apparatus, comprising: input/output means for transferring communication signals between an antenna and said demodulator/modulator apparatus; an up/down conversion means connected in series with said input/output means for converting received signals at extra high frequencies to a first preselected intermediate frequency range and for converting transmitted signals in said first intermediate frequency range to said extra high frequencies; tunable band pass filter connected in series with said up/ own conversion means, said tunable bandpass filter capable of having a preselected band pass range tuned in response to a control signal; a power signal splitter connected in series with said tunable band pass filter having three input/output ports with one connected to said tunable band pass filter; a first mixer connected at a first input to a second input/output port for said signal splitter; a coarse frequency synthesizer connected to said first mixer at a second input; a second band pass filter in series with said first mixer and connected to an output thereof; a second mixer connected in series with said second band pass filter and connected thereto at a first input; fine frequency synthesizer connected to said second mixer at a second input; a crystal output filter connected to an output of said second mixer; a third mixer connected at a first input to said fine synthesizer and at a second input to said coarse synthesizer, and having an output connected to a third input/output port of said power splitter; and transmit modulation means connected to said fine synthesizer for modulating a frequency output thereof in response to transmission of desired second communication signals.
PCT/US1988/004621 1988-01-19 1988-12-21 Alternating sequential half duplex communication system WO1989006883A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP89902364A EP0417099B1 (en) 1988-01-19 1988-12-21 Alternating sequential half duplex communication system
JP1502240A JP2974350B2 (en) 1988-01-19 1988-12-21 Alternating sequential half-duplex communication system
JP89502240A JPH03502392A (en) 1988-01-19 1988-12-21 Alternating sequential half-duplex communication system
AU30597/89A AU624120B2 (en) 1988-01-19 1988-12-21 Alternating sequential half duplex communication system
DE3855894T DE3855894T2 (en) 1988-01-19 1988-12-21 ALTERNATING SEQUENTIAL HALF DUPLEX TRANSMISSION SYSTEM
HK98107081A HK1008130A1 (en) 1988-01-19 1998-06-26 Alternating sequential half duplex communication system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/145,176 US4979170A (en) 1988-01-19 1988-01-19 Alternating sequential half duplex communication system
US145,176 1988-01-19

Publications (1)

Publication Number Publication Date
WO1989006883A1 true WO1989006883A1 (en) 1989-07-27

Family

ID=22511938

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1988/004621 WO1989006883A1 (en) 1988-01-19 1988-12-21 Alternating sequential half duplex communication system

Country Status (10)

Country Link
US (1) US4979170A (en)
EP (1) EP0417099B1 (en)
JP (1) JP2974350B2 (en)
AT (1) ATE152559T1 (en)
AU (2) AU3059789A (en)
CA (1) CA1310696C (en)
DE (1) DE3855894T2 (en)
HK (1) HK1008130A1 (en)
SG (1) SG48270A1 (en)
WO (1) WO1989006883A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0408587A1 (en) * 1988-01-19 1991-01-23 Qualcomm Inc Multiplexed address control in a tdm communication system.
WO1996019049A1 (en) * 1994-12-12 1996-06-20 Ericsson Inc. Diversity-oriented channel allocation in a mobile communications system
WO2016196142A1 (en) * 2015-05-31 2016-12-08 Hughes Network Systems, Llc Half-duplex communications for a very small aperture terminal (vsat) operating on a continuous stream

Families Citing this family (165)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303286A (en) * 1991-03-29 1994-04-12 Space Systems/Loral, Inc. Wireless telephone/satellite roaming system
US5638375A (en) * 1988-11-30 1997-06-10 Motorola, Inc. AGC isolation of information in TDMA systems
US5274836A (en) * 1989-08-08 1993-12-28 Gde Systems, Inc. Multiple encoded carrier data link
IE78845B1 (en) * 1990-02-27 1998-03-11 Motorola Inc Shared-carrier frequency-hopping
US5327572A (en) * 1990-03-06 1994-07-05 Motorola, Inc. Networked satellite and terrestrial cellular radiotelephone systems
US5446756A (en) * 1990-03-19 1995-08-29 Celsat America, Inc. Integrated cellular communications system
US5073900A (en) * 1990-03-19 1991-12-17 Mallinckrodt Albert J Integrated cellular communications system
US6749122B1 (en) * 1990-05-25 2004-06-15 Broadcom Corporation Multi-level hierarchial radio-frequency system communication system
JP3190660B2 (en) * 1990-06-13 2001-07-23 ソニー株式会社 Message transmission system
US5303393A (en) * 1990-11-06 1994-04-12 Radio Satellite Corporation Integrated radio satellite response system and method
US5402413A (en) * 1991-04-08 1995-03-28 Omnipoint Corporation Three-cell wireless communication system
US5796772A (en) * 1991-05-13 1998-08-18 Omnipoint Corporation Multi-band, multi-mode spread-spectrum communication system
US5790587A (en) * 1991-05-13 1998-08-04 Omnipoint Corporation Multi-band, multi-mode spread-spectrum communication system
US5887020A (en) * 1991-05-13 1999-03-23 Omnipoint Corporation Multi-band, multi-mode spread-spectrum communication system
US5815525A (en) * 1991-05-13 1998-09-29 Omnipoint Corporation Multi-band, multi-mode spread-spectrum communication system
US5694414A (en) * 1991-05-13 1997-12-02 Omnipoint Corporation Multi-band, multi-mode spread-spectrum communication system
US5285469A (en) * 1991-06-03 1994-02-08 Omnipoint Data Corporation Spread spectrum wireless telephone system
US5526404A (en) * 1991-10-10 1996-06-11 Space Systems/Loral, Inc. Worldwide satellite telephone system and a network coordinating gateway for allocating satellite and terrestrial gateway resources
CN1038174C (en) * 1991-11-12 1998-04-22 美国西塞特公司 Integrated cellular communications system
JP3766434B2 (en) * 1991-12-16 2006-04-12 ザーカム ワイヤレス， インコーポレイテッド Spread spectrum data transmission system
US5737685A (en) * 1992-02-25 1998-04-07 Motorola, Inc. Co-located subscriber unit to subscriber unit communication within a satellite communication system
US5444762A (en) * 1993-03-08 1995-08-22 Aircell, Inc. Method and apparatus for reducing interference among cellular telephone signals
US5832380A (en) * 1992-03-06 1998-11-03 Aircell Incorporated Nonterrestrial cellular mobile telecommunication system
US5878346A (en) * 1992-03-06 1999-03-02 Aircell Incorporated Nonterrestrial cellular mobile telecommunication network
US5878345A (en) * 1992-03-06 1999-03-02 Aircell, Incorporated Antenna for nonterrestrial mobile telecommunication system
US5884166A (en) * 1992-03-06 1999-03-16 Aircell, Incorporated Multidimensional cellular mobile telecommunication system
US5263047A (en) * 1992-07-02 1993-11-16 Motorola, Inc. Multiple cavity tuning of a transmitter output in a communication system
US5410315A (en) * 1992-12-08 1995-04-25 Texas Instruments Incorporated Group-addressable transponder arrangement
US5708679A (en) * 1993-03-11 1998-01-13 Southern California Edison Company Hitless ultra small aperture terminal satellite communication network
US6366244B1 (en) 1993-03-11 2002-04-02 Southern California Edison Company Planar dual band microstrip or slotted waveguide array antenna for all weather applications
US5594936A (en) * 1993-04-16 1997-01-14 Trans Video Electronics, Inc. Global digital video news distribution system
US6175717B1 (en) 1993-04-16 2001-01-16 Trans Video Electronics, Inc. Global mobile video communications system
US7397363B2 (en) * 1993-06-08 2008-07-08 Raymond Anthony Joao Control and/or monitoring apparatus and method
US6094575A (en) * 1993-11-01 2000-07-25 Omnipoint Corporation Communication system and method
JP3692140B2 (en) * 1993-11-01 2005-09-07 オムニポイント・コーポレイション Dual-mode wireless device having two spread spectrum frequency bands
US6005856A (en) * 1993-11-01 1999-12-21 Omnipoint Corporation Communication protocol for spread spectrum wireless communication system
US5666379A (en) * 1993-11-01 1997-09-09 Omnipoint Corporation Best-of-M pulse position modulation detector
US6088590A (en) * 1993-11-01 2000-07-11 Omnipoint Corporation Method and system for mobile controlled handoff and link maintenance in spread spectrum communication
US5654978A (en) * 1993-11-01 1997-08-05 Omnipoint Corporation Pulse position modulation with spread spectrum
US5594720A (en) * 1993-11-24 1997-01-14 Lucent Technologies Inc. Multiple access cellular communication with dynamic slot allocation and reduced co-channel interferences
US5420851A (en) * 1993-11-24 1995-05-30 At&T Corp. Method of multiple access
US5602836A (en) * 1993-11-24 1997-02-11 Lucent Technologies Inc. Multiple access cellular communication with circular interleaving and reduced dropped-packet runlengths
US5434548A (en) * 1994-03-28 1995-07-18 Qualcomm Incorporated Coaxial-waveguide rotary coupling assemblage
AU2291195A (en) * 1994-04-12 1995-10-30 Qualcomm Incorporated Method and apparatus for freight transportation using a satellite navigation system
US5610906A (en) * 1994-06-29 1997-03-11 Interdigital Technology Corporation Spread-spectrum changeable base station
JP2606145B2 (en) * 1994-08-15 1997-04-30 日本電気株式会社 Satellite communication system
EP0728383B1 (en) 1994-09-14 2007-08-22 Ericsson Inc. Satellite communications adapter for cellular handset
US5625640A (en) * 1994-09-16 1997-04-29 Hughes Electronics Apparatus for and method of broadcast satellite network return-link signal transmission
BR9510253B1 (en) * 1994-12-19 2009-01-13 process and system for communicating message information to a driver and system and process for displaying messages within a vehicle.
US5734966A (en) * 1995-01-20 1998-03-31 Diablo Research Corporation Wireless communication system for adapting to frequency drift
US5959980A (en) * 1995-06-05 1999-09-28 Omnipoint Corporation Timing adjustment control for efficient time division duplex communication
US5745484A (en) * 1995-06-05 1998-04-28 Omnipoint Corporation Efficient communication system using time division multiplexing and timing adjustment control
US5689502A (en) * 1995-06-05 1997-11-18 Omnipoint Corporation Efficient frequency division duplex communication system with interleaved format and timing adjustment control
US5802046A (en) * 1995-06-05 1998-09-01 Omnipoint Corporation Efficient time division duplex communication system with interleaved format and timing adjustment control
ZA965340B (en) 1995-06-30 1997-01-27 Interdigital Tech Corp Code division multiple access (cdma) communication system
US7020111B2 (en) 1996-06-27 2006-03-28 Interdigital Technology Corporation System for using rapid acquisition spreading codes for spread-spectrum communications
US6885652B1 (en) 1995-06-30 2005-04-26 Interdigital Technology Corporation Code division multiple access (CDMA) communication system
US7929498B2 (en) 1995-06-30 2011-04-19 Interdigital Technology Corporation Adaptive forward power control and adaptive reverse power control for spread-spectrum communications
US7123600B2 (en) 1995-06-30 2006-10-17 Interdigital Technology Corporation Initial power control for spread-spectrum communications
JPH0918378A (en) * 1995-07-03 1997-01-17 Matsushita Electric Ind Co Ltd Radio circuit
US6041046A (en) * 1995-07-14 2000-03-21 Omnipoint Corporation Cyclic time hopping in time division multiple access communication system
US5592175A (en) * 1995-08-25 1997-01-07 Motorola, Inc. Location determination method and apparatus for a communication unit
US5652750A (en) * 1995-08-28 1997-07-29 Ericsson Inc. Optical satellite feeder links
US5768254A (en) * 1995-09-29 1998-06-16 Lucent Technologies Inc. Multiple access cellular communication with signal cancellation to reduce co-channel interference
JP3212854B2 (en) * 1995-11-30 2001-09-25 三菱電機株式会社 Antenna initial value setting device, initial value setting method, and satellite communication system
US7590083B2 (en) * 1995-12-07 2009-09-15 Transcore Link Logistics Corp. Wireless packet data distributed communications system
WO1997021281A1 (en) * 1995-12-08 1997-06-12 Amsc Subsidiary Corporation Mobile communications terminal for satellite communications system
US6100792A (en) * 1996-05-20 2000-08-08 Alpine Electronics, Inc. Car security apparatus and car security system
US6084870A (en) * 1996-07-22 2000-07-04 Qualcomm Incorporated Method and apparatus for the remote monitoring and configuration of electronic control systems
US5918158A (en) * 1996-07-24 1999-06-29 Lucent Technologies Inc. Two-way wireless messaging system
US5937332A (en) * 1997-03-21 1999-08-10 Ericsson, Inc. Satellite telecommunications repeaters and retransmission methods
US6243366B1 (en) * 1997-06-20 2001-06-05 At&T Corp. Method and apparatus for providing interactive two-way communications using a single one-way channel in satellite systems
US6073007A (en) 1997-07-24 2000-06-06 Qualcomm Incorporated Wireless fleet communications system for providing separable communications services
JPH1141132A (en) * 1997-07-24 1999-02-12 Toshiba Corp Radio communication device
US6026292A (en) * 1997-08-19 2000-02-15 Qualcomm Incorporated Truck communication system
US5991615A (en) * 1997-08-18 1999-11-23 Transcommunications, Inc. Truck communication system
US5940739A (en) * 1997-10-24 1999-08-17 Conrad; Charles Multiple access satellite communications network
US7006788B1 (en) 1997-12-11 2006-02-28 Dyncorp Information Systems Llc Method and system for preventing sun transit outages in point-to-multipoint satellite systems
US7020103B1 (en) * 1998-03-26 2006-03-28 Ericsson Inc. Broadband communication system using point and shoot approach
US6515976B1 (en) * 1998-04-06 2003-02-04 Ericsson Inc. Demodulation method and apparatus in high-speed time division multiplexed packet data transmission
US6181931B1 (en) * 1998-08-28 2001-01-30 Qualcomm Inc. Method and apparatus for dynamic address allocation in a wireless communication system
CN1183467C (en) * 1998-08-31 2005-01-05 株式会社神户制钢所 Management system for construction machinery
US6124810A (en) 1998-09-15 2000-09-26 Qualcomm Incorporated Method and apparatus for automatic event detection in a wireless communication system
GB9826665D0 (en) * 1998-12-03 1999-01-27 Nokia Telecommunications Oy A receiver and method of receiving
FR2786937B1 (en) * 1998-12-04 2001-02-16 Photonetics MULTI-WAVELENGTH SOURCE
US7215954B1 (en) 1999-03-18 2007-05-08 The Directv Group, Inc. Resource allocation method for multi-platform communication system
US6920309B1 (en) 1999-03-18 2005-07-19 The Directv Group, Inc. User positioning technique for multi-platform communication system
GB9909196D0 (en) * 1999-04-21 1999-06-16 Texas Instruments Ltd Transfer controller with hub and ports architecture
US6947469B2 (en) 1999-05-07 2005-09-20 Intel Corporation Method and Apparatus for wireless spread spectrum communication with preamble processing period
FR2793631B1 (en) * 1999-05-10 2001-07-27 Centre Nat Etd Spatiales MULTMEDIA BIDIRECTIONAL COMMUNICATION TERMINAL
US6422628B1 (en) * 1999-05-10 2002-07-23 Veridian Erim International, Inc. Transportable satellite communication station including double-expandable trailer
AU5588000A (en) * 1999-05-19 2000-12-05 Id Systems, Inc. Fully automated vehicle rental system
US7656271B2 (en) * 2002-01-09 2010-02-02 I.D. Systems, Inc. System and method for managing a remotely located asset
US20080015955A1 (en) * 1999-05-19 2008-01-17 I.D. Systems, Inc. Mobile asset data management system
US7356494B2 (en) * 1999-05-19 2008-04-08 I.D. Systems, Inc. Robust wireless communications system architecture and asset management applications performed thereon
WO2002087112A2 (en) 2001-04-18 2002-10-31 Space Data Corporation Unmanned lighter-than-air safe termination and recovery methods
US6628941B2 (en) 1999-06-29 2003-09-30 Space Data Corporation Airborne constellation of communications platforms and method
US7356390B2 (en) * 1999-06-29 2008-04-08 Space Data Corporation Systems and applications of lighter-than-air (LTA) platforms
US7215650B1 (en) * 1999-08-16 2007-05-08 Viasat, Inc. Adaptive data rate control for narrowcast networks
US7068147B2 (en) * 1999-12-07 2006-06-27 Denso Corporation Control information rewriting system
US7339520B2 (en) * 2000-02-04 2008-03-04 The Directv Group, Inc. Phased array terminal for equatorial satellite constellations
WO2001065876A1 (en) * 2000-02-29 2001-09-07 Qualcomm Incorporated Programmable mobile communications terminal with randomized off-peak transmissions
US20010043573A1 (en) * 2000-04-14 2001-11-22 Frank Kelly System and method for providing control of a two-way satellite system
US6963548B1 (en) 2000-04-17 2005-11-08 The Directv Group, Inc. Coherent synchronization of code division multiple access signals
US6388615B1 (en) 2000-06-06 2002-05-14 Hughes Electronics Corporation Micro cell architecture for mobile user tracking communication system
US6756937B1 (en) 2000-06-06 2004-06-29 The Directv Group, Inc. Stratospheric platforms based mobile communications architecture
US6859652B2 (en) 2000-08-02 2005-02-22 Mobile Satellite Ventures, Lp Integrated or autonomous system and method of satellite-terrestrial frequency reuse using signal attenuation and/or blockage, dynamic assignment of frequencies and/or hysteresis
US6892068B2 (en) 2000-08-02 2005-05-10 Mobile Satellite Ventures, Lp Coordinated satellite-terrestrial frequency reuse
US7092803B2 (en) * 2000-08-18 2006-08-15 Idsc Holdings, Llc Remote monitoring, configuring, programming and diagnostic system and method for vehicles and vehicle components
US6771615B1 (en) * 2000-08-18 2004-08-03 Hughes Electronics Corporation Synchronization apparatus and method for a return link power control for satellite systems
US6763242B1 (en) 2000-09-14 2004-07-13 The Directv Group, Inc. Resource assignment system and method for determining the same
US7792488B2 (en) 2000-12-04 2010-09-07 Atc Technologies, Llc Systems and methods for transmitting electromagnetic energy over a wireless channel having sufficiently weak measured signal strength
US6952580B2 (en) 2000-12-12 2005-10-04 The Directv Group, Inc. Multiple link internet protocol mobile communications system and method therefor
US6891813B2 (en) 2000-12-12 2005-05-10 The Directv Group, Inc. Dynamic cell CDMA code assignment system and method
US7103317B2 (en) * 2000-12-12 2006-09-05 The Directv Group, Inc. Communication system using multiple link terminals for aircraft
US7400857B2 (en) 2000-12-12 2008-07-15 The Directv Group, Inc. Communication system using multiple link terminals
US7181162B2 (en) 2000-12-12 2007-02-20 The Directv Group, Inc. Communication system using multiple link terminals
US7068733B2 (en) * 2001-02-05 2006-06-27 The Directv Group, Inc. Sampling technique for digital beam former
US6559797B1 (en) 2001-02-05 2003-05-06 Hughes Electronics Corporation Overlapping subarray patch antenna system
US9632503B2 (en) 2001-04-18 2017-04-25 Space Data Corporation Systems and applications of lighter-than-air (LTA) platforms
US9908608B2 (en) 2001-04-18 2018-03-06 Space Data Corporation Systems and applications of lighter-than-air (LTA) platforms
US9643706B2 (en) 2001-04-18 2017-05-09 Space Data Corporation Systems and applications of lighter-than-air (LTA) platforms
US7155321B2 (en) 2001-08-06 2006-12-26 Idsc Holdings Llc System, method and computer program product for remote vehicle diagnostics, monitoring, configuring and reprogramming
US7068704B1 (en) * 2001-09-26 2006-06-27 Itt Manufacturing Enterpprises, Inc. Embedded chirp signal for position determination in cellular communication systems
US7212984B2 (en) * 2001-10-29 2007-05-01 Qualcomm Incorporated Method and apparatus for providing virtual capacity to a provider of services
US7765297B2 (en) * 2001-11-13 2010-07-27 Qualcomm Incorporated System for providing online service reports
KR100450815B1 (en) * 2002-02-01 2004-10-01 삼성전자주식회사 Illumination system and projection display device employing it
US20030162523A1 (en) * 2002-02-27 2003-08-28 Michael Kapolka Vehicle telemetry system and method
US7730208B2 (en) * 2002-05-09 2010-06-01 Hughes Network Systems, Inc. Method and system for centrally exchanging terminal information over a meshed network
US20040114625A1 (en) * 2002-10-25 2004-06-17 Roundy Larry Lee Method and apparatus for simultaneous incoming digital call processing using H.221 protocol
US20050029872A1 (en) * 2003-08-08 2005-02-10 Ehrman Kenneth S. Universal power supply
WO2006093992A2 (en) * 2005-03-01 2006-09-08 I.D. Systems, Inc. Mobile portal for rfid applications
US7786844B2 (en) * 2005-03-01 2010-08-31 I.D. Systems, Inc. Mobile portal for RFID applications
KR100677481B1 (en) * 2005-08-04 2007-02-02 엘지전자 주식회사 Apparatus for common antenna of mobile terminal built-in rfid function and method thereof
US20070120664A1 (en) * 2005-11-30 2007-05-31 Syncro Corporation Fire hydrant locating system
DE102006021100A1 (en) * 2006-05-05 2007-11-08 Benq Mobile Gmbh & Co. Ohg Method for transmitting data in a radio network, radio network and receiver
WO2008030770A2 (en) * 2006-09-07 2008-03-13 Qualcomm Incorporated Hardware continuity loop for preventing vehicle misappropriation
US7760077B2 (en) * 2007-06-05 2010-07-20 Qualcomm Incorporated Establishing and securing a unique wireless RF link between a tractor and a trailer using a wired connection
US9305405B2 (en) * 2007-06-26 2016-04-05 Omnitracs, Llc Reefer fuel tax reporting for the transport industry
US8023886B2 (en) * 2007-09-28 2011-09-20 Broadcom Corporation Method and system for repeater with gain control and isolation via polarization
US7881753B2 (en) * 2007-09-28 2011-02-01 Broadcom Corporation Method and system for sharing multiple antennas between TX and RX in a repeat field of polarization isolation
US20090128291A1 (en) * 2007-11-19 2009-05-21 Broadcom Corporation Method and apparatus of rfid communication during device assembly
FR2936674B1 (en) 2008-09-26 2010-11-05 Centre Nat Etd Spatiales TRANSMISSION ACCESS METHOD WITHOUT FREQUENCY DUPLEXER
US8682956B2 (en) * 2011-06-09 2014-03-25 Gm Global Technology Operations, Inc Systems and methods for determining recommended media content for exchange between vehicles
US9576046B2 (en) 2011-11-16 2017-02-21 Ptc Inc. Methods for integrating semantic search, query, and analysis across heterogeneous data types and devices thereof
US8909641B2 (en) 2011-11-16 2014-12-09 Ptc Inc. Method for analyzing time series activity streams and devices thereof
US9098312B2 (en) 2011-11-16 2015-08-04 Ptc Inc. Methods for dynamically generating an application interface for a modeled entity and devices thereof
CN102843178B (en) * 2012-07-27 2014-12-17 航天东方红卫星有限公司 Spread spectrum relay measurement and control system compatible with standard unified S-band measurement and control system
WO2014145084A1 (en) 2013-03-15 2014-09-18 Ptc Inc. Methods for managing applications using semantic modeling and tagging and devices thereof
US9762637B2 (en) 2014-03-21 2017-09-12 Ptc Inc. System and method of using binary dynamic rest messages
US9961058B2 (en) 2014-03-21 2018-05-01 Ptc Inc. System and method of message routing via connection servers in a distributed computing environment
US9350812B2 (en) 2014-03-21 2016-05-24 Ptc Inc. System and method of message routing using name-based identifier in a distributed computing environment
US9560170B2 (en) 2014-03-21 2017-01-31 Ptc Inc. System and method of abstracting communication protocol using self-describing messages
US10338896B2 (en) 2014-03-21 2019-07-02 Ptc Inc. Systems and methods for developing and using real-time data applications
US9467533B2 (en) 2014-03-21 2016-10-11 Ptc Inc. System and method for developing real-time web-service objects
US9462085B2 (en) 2014-03-21 2016-10-04 Ptc Inc. Chunk-based communication of binary dynamic rest messages
US9350791B2 (en) 2014-03-21 2016-05-24 Ptc Inc. System and method of injecting states into message routing in a distributed computing environment
US10025942B2 (en) 2014-03-21 2018-07-17 Ptc Inc. System and method of establishing permission for multi-tenancy storage using organization matrices
US10313410B2 (en) 2014-03-21 2019-06-04 Ptc Inc. Systems and methods using binary dynamic rest messages
WO2016105522A1 (en) 2014-12-24 2016-06-30 Space Data Corporation Breaking apart a platform upon pending collision
WO2016105523A1 (en) 2014-12-24 2016-06-30 Space Data Corporation Techniques for intelligent balloon/airship launch and recovery window location
US10059421B2 (en) 2014-12-30 2018-08-28 Space Data Corporation Multifunctional balloon membrane
KR102324960B1 (en) 2015-06-25 2021-11-12 삼성전자 주식회사 Communication device and electronic device including the same
US11280880B2 (en) 2019-11-21 2022-03-22 Rockwell Collins, Inc. Single channel dual orthogonal linear polarization array
US11239904B2 (en) * 2020-02-11 2022-02-01 Ast & Science, Llc Geolocation of radio frequency devices using spaceborne phased arrays

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4117267A (en) * 1976-04-08 1978-09-26 International Standard Electric Corporation System for two-way communication between a master station and a plurality of substations via a satellite
US4288868A (en) * 1978-06-20 1981-09-08 U.S. Philips Corporation Satellite communication system for speech and telegraphy
US4504946A (en) * 1982-06-11 1985-03-12 Rca Corporation Time division multiple access communication systems
US4736371A (en) * 1985-12-30 1988-04-05 Nec Corporation Satellite communications system with random multiple access and time slot reservation

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4009343A (en) * 1974-12-30 1977-02-22 International Business Machines Corporation Switching and activity compression between telephone lines and digital communication channels
US4172214A (en) * 1977-03-25 1979-10-23 Trw Inc. Integrated message accounting system
US4288862A (en) * 1977-12-21 1981-09-08 Nippon Telegraph And Telephone Public Corp. Memory circuit
US4287588A (en) * 1979-04-12 1981-09-01 The United States Of America As Represented By The Secretary Of The Army Multiple access, time-division multiplex, satellite communications system
US4309764A (en) * 1979-06-22 1982-01-05 Bell Telephone Laboratories, Incorporated Technique for increasing the rain margin of a satellite communication system
US4408322A (en) * 1980-11-07 1983-10-04 Satellite Business Systems Method and apparatus for measuring signal to noise ratio in a TDMA communications system
GB2118337B (en) * 1982-02-09 1986-01-15 Nippon Electric Co Pager receiver for giving at least one of extraordinary tones and extraordinary displays
US4625308A (en) * 1982-11-30 1986-11-25 American Satellite Company All digital IDMA dynamic channel allocated satellite communications system and method
US4686672A (en) * 1983-10-13 1987-08-11 Nec Corporation TDMA communications apparatus having adaptive burst duration
US4549303A (en) * 1983-12-27 1985-10-22 The United States Of America As Represented By The Secretary Of The Army Multichannel time division multiplexed trunk transmission link
US4686673A (en) * 1984-02-15 1987-08-11 Toshinori Hotta Synchronizing burst transmission phase control system
US4608684A (en) * 1984-03-26 1986-08-26 Itt Corporation Digital switching systems employing multi-channel frame association apparatus
US4581749A (en) * 1984-07-02 1986-04-08 Motorola, Inc. Data frequency modulator with deviation control
JPS61120538A (en) * 1984-11-15 1986-06-07 Nec Corp Multi-direction multiplex communication equipment
US4713808A (en) * 1985-11-27 1987-12-15 A T & E Corporation Watch pager system and communication protocol
US4675863A (en) * 1985-03-20 1987-06-23 International Mobile Machines Corp. Subscriber RF telephone system for providing multiple speech and/or data signals simultaneously over either a single or a plurality of RF channels
US4617658A (en) * 1985-04-17 1986-10-14 Bell Communications Research, Inc. Frame arrangement for multiplexing a plurality of subchannels onto a fixed rate channel
NL8502023A (en) * 1985-07-15 1987-02-02 Philips Nv METHOD FOR SWITCHING TIME LOCKS IN A TDM SIGNAL AND APPARATUS FOR PERFORMING THE METHOD
DE3527330A1 (en) * 1985-07-31 1987-02-05 Philips Patentverwaltung DIGITAL RADIO TRANSMISSION SYSTEM WITH CONNECTING ORGANIZATION CHANNEL IN THE TIME MULTIPLEX FRAME
US4646294A (en) * 1985-08-02 1987-02-24 Gte Laboratories Incorporated High-speed queue sequencer for a burst-switching communications system
US4644529A (en) * 1985-08-02 1987-02-17 Gte Laboratories Incorporated High-speed switching processor for a burst-switching communications system
US4928274A (en) * 1988-01-19 1990-05-22 Qualcomm, Inc. Multiplexed address control in a TDM communication system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4117267A (en) * 1976-04-08 1978-09-26 International Standard Electric Corporation System for two-way communication between a master station and a plurality of substations via a satellite
US4288868A (en) * 1978-06-20 1981-09-08 U.S. Philips Corporation Satellite communication system for speech and telegraphy
US4504946A (en) * 1982-06-11 1985-03-12 Rca Corporation Time division multiple access communication systems
US4736371A (en) * 1985-12-30 1988-04-05 Nec Corporation Satellite communications system with random multiple access and time slot reservation

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0408587A1 (en) * 1988-01-19 1991-01-23 Qualcomm Inc Multiplexed address control in a tdm communication system.
EP0408587A4 (en) * 1988-01-19 1992-08-19 Qualcomm, Inc. Multiplexed address control in a tdm communication system
WO1996019049A1 (en) * 1994-12-12 1996-06-20 Ericsson Inc. Diversity-oriented channel allocation in a mobile communications system
US5841766A (en) * 1994-12-12 1998-11-24 Ericsson Inc. Diversity-oriented channel allocation in a mobile communications system
WO2016196142A1 (en) * 2015-05-31 2016-12-08 Hughes Network Systems, Llc Half-duplex communications for a very small aperture terminal (vsat) operating on a continuous stream
US9853717B2 (en) 2015-05-31 2017-12-26 Hughes Network Systems, L.L.C. Half-duplex communications for a very small aperture terminal (VSAT) operating on a continuous stream

Also Published As

Publication number Publication date
US4979170A (en) 1990-12-18
EP0417099A1 (en) 1991-03-20
SG48270A1 (en) 1998-04-17
JP2974350B2 (en) 1999-11-10
AU1295792A (en) 1992-05-21
AU3059789A (en) 1989-08-11
DE3855894D1 (en) 1997-06-05
HK1008130A1 (en) 1999-04-30
EP0417099A4 (en) 1991-07-31
ATE152559T1 (en) 1997-05-15
CA1310696C (en) 1992-11-24
DE3855894T2 (en) 1997-12-11
AU640561B2 (en) 1993-08-26
JPH01502619A (en) 1989-09-07
EP0417099B1 (en) 1997-05-02

Similar Documents

Publication Publication Date Title
US4979170A (en) Alternating sequential half duplex communication system
US4928274A (en) Multiplexed address control in a TDM communication system
US6118824A (en) Spread-spectrum data publishing system
US5218618A (en) Cellular telephone service using spread spectrum transmission
US5390166A (en) Method for recovering a data signal using diversity in a radio frequency, time division multiple access communication system
US5926758A (en) Radio frequency sharing methods for satellite systems
AU612308B2 (en) Cellular data system
US6519262B1 (en) Time division multiplex approach for multiple transmitter broadcasting
JP3853359B2 (en) MESSAGE DEVICE HAVING CHANNEL ALLOCATION TABLE USED FOR MULTI-BEAM SATELLITE MESSAGE SYSTEM AND ITS OPERATION METHOD
EP1040590B1 (en) Increased capacity in an ocdma system by frequency isolation
WO1990013186A1 (en) Communication system employing multiple relay satellites operating on common downlink frequency
EP0746120B1 (en) Communication system with repeatedly allocated channel ID numbers
AU624120B2 (en) Alternating sequential half duplex communication system
EP0976277A2 (en) Method of facilitating transmission level measurement, and base station
RU2227371C2 (en) High-efficiency and high-altitude suborbital telecommunication system and method for establishing wireless telecommunications
Huang et al. Communication satellite processing repeaters
JP2000502863A (en) High power short message service using TDMA frame
Jacobs et al. A second anniversary operational review of the OmniTRACS (R): The first two-way mobile Ku-band satellite communications system
US20040152452A1 (en) Paging method and apparatus with acknowledgement capability
WO1998031110A1 (en) Method for improving system capacity in a cellular radio system, and a base station
Hemmati A C-band micro-terminal
Milcz Change-over strategies for highly elliptical orbits
WO1999027655A2 (en) Method for connection establishment, and transceiver
Toshinaga et al. Bi-directional multimedia satellite communication system employing superposed transmission
Furman et al. UHF (Ultra High Frequency) Military Satellite Communications Ground Equipment Interoperability.

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AU JP

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LU NL SE

WWE Wipo information: entry into national phase

Ref document number: 1989902364

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 1989902364

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1989902364

Country of ref document: EP