US3910192A - Fuze signal processing circuit - Google Patents

Fuze signal processing circuit Download PDF

Info

Publication number
US3910192A
US3910192A US370740A US37074064A US3910192A US 3910192 A US3910192 A US 3910192A US 370740 A US370740 A US 370740A US 37074064 A US37074064 A US 37074064A US 3910192 A US3910192 A US 3910192A
Authority
US
United States
Prior art keywords
controlled rectifier
silicon controlled
target envelope
storage capacitor
signal
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
US370740A
Inventor
John O Dick
Jr John C Billings
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Department of Navy
Original Assignee
US Department of Navy
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 US Department of Navy filed Critical US Department of Navy
Priority to US370740A priority Critical patent/US3910192A/en
Application granted granted Critical
Publication of US3910192A publication Critical patent/US3910192A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00Proximity fuzes; Fuzes for remote detonation
    • F42C13/02Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation

Definitions

  • said silicon controlled rectifier being serially connected across said storage capacitor
  • circuit means coupling the anode of said silicon controlled rectifier to said output terminal
  • circuit means including a Zener diode coupled to 1 Claim, 4 Drawing Figures US. Patem Oct. 7,1975 3,910,192
  • the present invention relates to that portion of a passive infrared actuated type fuzing system that processes the intercepted signal and makes the decision as to the correct time to actuate the firing of the missile warhead.
  • the signal shape in general is that of a sawtooth or exponentially increasing voltage waveform.
  • the termination of the waveform (as the detector passes the jet engine tailpipe) is a sharply decreasing fall off to zero as the IR source seen by the detector disappears from the detector field of view.
  • Prior circuitry has simply differentiated this waveform by means of a resistor-capacitor coupling network to select the sharp voltage transition occurring at intercept.
  • the target envelope as seen by the detector may not be the clean waveform as previously assumed. Recent tests have disclosed the fact that the target envelope of the jet engine exhaust plume may contain a high degree of modulation (up to 40 percent).
  • the magnitude of the modulation spikes described above may be much larger than the minimum signal necessary to produce fuze actuation.
  • the signal processing circuitry can distinguish between a true signal and the above modulation. The result of this is that the fuze may fire prematurely upon the modulation and thus fail to destroy the intended target.
  • Prior fuzing systems utilize the trailing edge of the intercept signal waveform as a timing reference point for detonating the missile warhead.
  • the trailing edge of the signal is located by differentiation of the intercept signal in a resistor-capacitor coupling network.
  • An object of the present invention is to provide a fuze signal processing circuit which is not influenced by the high degree of modulation present in the target envelope signal as a result of the jet engine exhaust plume.
  • Another object of the invention is the provision of a fuze signal processing circuit that assures a more precise point of firing of the fuze by accurately detennining the exact point of signal fall off.
  • a further object is to provide a fuze signal processing circuit that minimizes the probability of dudding due to long pulse width signals obtained during slow-missileto-target overtake velocities.
  • FIG. 1 shows a schematic diagram of a preferred embodimcnt of the processing circuit.
  • FIG. 2 shows a modification of the circuit of FIG. 1.
  • FIG. 3 shows a further modification of the circuit of FIG. 1.
  • FIG. 4 shows graphically the point of firing of the circuit of FIG. 1.
  • FIG. 1 the final amplifier stage 10- of an IR fuzing system (not shown) which provides the signal Wavefrom A; Because of the large modulation or'serrations present in Waveform A, a resistor-capacitor differentiating circuit would produce a premature pulse which would fire the fuze.
  • Waveform signal A is coupled through coupling capacitor 12 and diode 14 to charge capacitor 16 with a voltage as illustrated by Waveform C.
  • Diode 14 is polarized so that a negative going signal is passed by the forward conductance of diode 14 but positive signals are blocked, thus, storing the negative peaks of Waveform A in capacitor 16.
  • the peak amplitude of the signal is stored in capacitor 16 and held by choosing the values of capacitor 16 and resistor 18 to have long time constant.
  • Waveform signal A is also coupled through coupling capacitor 20, with a small amount of integration as shown by Waveform B, and Zener Diode 22 to the control electrode of silicon controlled rectifier 24. As shown in FIG. 4, there is no voltage difference across Diode 22 so that it does not conduct.
  • Waveform B drops to zero, the voltage across Diode 22 increases until its breakdown voltage (V FIG. 4) is exceeded and it begins to conduct.
  • This diode current is applied to the control electrode of controlled rectifier 24 and causes it to switch, thereby discharging capacitor 16 and producing a precise trigger pulse at terminal 28 to mark the termination of the detected signal.
  • the portion 30 of Waveform C is the nor mal decay of resistor 18 and capacitor 16 time constant while the portion 32 shows the discharge when controlled rectifier 24 is switched on.
  • FIG. 2 is functionally the same as FIG. 1 but has been modified by replacing the dual coupling capacitors 12 and 20 with a single coupling capacitor 36.
  • FIG. 3 is functionally the same as FIG. 1 with the ad dition of diode 38 and integrating capacitor 40 to prevent narrow spikes from inadvertently firing rectifier 24.
  • a fuze processing circuit which is not influenced by a high degree of modulation present in the target envelope signal, the combination comprising:
  • said silicon controlled rectifier being serially connected across said storage capacitor
  • circuit means coupling the anode of said silicon controlled rectifier to said output terminal

Abstract

1. In a fuze processing circuit which is not influenced by a high degree of modulation present in the target envelope signal, the combination comprising: A. A SOURCE OF TARGET ENVELOPE NEGATIVE SIGNALS HAVING A HIGH DEGREE OF MODULATION, B. A STORAGE CAPACITOR, C. A DIODE COUPLING ONLY THE NEGATIVE GOING PORTION AND BLOCKING THE POSITIVE GOING PORTIONS OF SAID TARGET ENVELOPE SIGNAL TO SAID STORAGE CAPACITOR, D. AN OUTPUT TERMINAL, E. A NORMALLY NON-CONDUCTING SILICON CONTROLLED RECTIFIER, F. SAID SILICON CONTROLLED RECTIFIER BEING SERIALLY CONNECTED ACROSS SAID STORAGE CAPACITOR, G. CIRCUIT MEANS COUPLING THE ANODE OF SAID SILICON CONTROLLED RECTIFIER TO SAID OUTPUT TERMINAL, H. CIRCUIT MEANS INCLUDING A Zener diode coupled to said source of target envelope negative signals and to the control electrode of said normally non-conducting silicon controlled rectifier for switching said normally non-conducting silicon controlled rectifier to a conducting condition to discharge said storage capacitor in response to the termination of a target envelope negative signal.

Description

Dick et al.
Oct. 7, 1975 FUZE SIGNAL PROCESSING CIRCUIT [75] Inventors: John Dick, Riverside; John C.
Billings, Jr., La Sierra, both of Calif.
[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
[22] Filed: May 27, 1964 [21] Appl. No.: 370,740
[52] .U.S. Cl. l02/70.2 P [51] Int. Cl. F42C 13/00 [58] Field of Search 102/702, 70.2 P; 307/885; 323/22 Z [56] References Cited UNITED STATES PATENTS 3,022,732 2/1962 Paley 102/702 P 3,173,077 3/1965 Kirk et a1. 323/22 Z 3,198,989 8/1965 Mahoney..... 307/885 3,236,239 2/1966 Berkovits..... 307/885 3,237,023 2/1966 Wilhelm 324/111 Primary Examiner-Samuel Feinberg Assistant Examiner-C. T. Jordan Attorney, Agent, or FirmRichard S. Sciascia; Joseph M. St.Amand; T. M. Phillips EXEMPLARY CLAIM 1. In a fuze processing circuit which is not influenced by a high degree of modulation present in the target envelope signal, the combination comprising:
a source of target envelope negative signals having a high degree of modulation,
a storage capacitor,
a diode coupling only the negative going portion and blocking the positive going portions of said target envelope signal to said storage capacitor,
. an output terminal,
. a normally non-conducting silicon controlled rectifier,
. said silicon controlled rectifier being serially connected across said storage capacitor,
. circuit means coupling the anode of said silicon controlled rectifier to said output terminal,
. circuit means including a Zener diode coupled to 1 Claim, 4 Drawing Figures US. Patem Oct. 7,1975 3,910,192
JOHN D. DICK JOHN C. BILLINGS JR.
INVENTORS ATTORNEYS FUZE SIGNAL PROCESSING CIRCUIT The invention herein described may be, manufactured and used by or for the Government of the United States of America forgovernm ental purposes without the payment of any royalties thereon or therefor.
The present invention relates to that portion of a passive infrared actuated type fuzing system that processes the intercepted signal and makes the decision as to the correct time to actuate the firing of the missile warhead.
In the past it has been assumed that the signal shape in general is that of a sawtooth or exponentially increasing voltage waveform. The termination of the waveform (as the detector passes the jet engine tailpipe) is a sharply decreasing fall off to zero as the IR source seen by the detector disappears from the detector field of view. Prior circuitry has simply differentiated this waveform by means of a resistor-capacitor coupling network to select the sharp voltage transition occurring at intercept.
It has recently been determined that the target envelope as seen by the detector may not be the clean waveform as previously assumed. Recent tests have disclosed the fact that the target envelope of the jet engine exhaust plume may contain a high degree of modulation (up to 40 percent).
Due to the wide dynamic range required in fuzing systems, the magnitude of the modulation spikes described above may be much larger than the minimum signal necessary to produce fuze actuation. In addition, due to the wide range of intercept velocities and signal pulse width, there is no way in which the signal processing circuitry can distinguish between a true signal and the above modulation. The result of this is that the fuze may fire prematurely upon the modulation and thus fail to destroy the intended target.
Prior fuzing systems utilize the trailing edge of the intercept signal waveform as a timing reference point for detonating the missile warhead. The trailing edge of the signal is located by differentiation of the intercept signal in a resistor-capacitor coupling network.
An object of the present invention is to provide a fuze signal processing circuit which is not influenced by the high degree of modulation present in the target envelope signal as a result of the jet engine exhaust plume.
Another object of the invention is the provision of a fuze signal processing circuit that assures a more precise point of firing of the fuze by accurately detennining the exact point of signal fall off.
A further object is to provide a fuze signal processing circuit that minimizes the probability of dudding due to long pulse width signals obtained during slow-missileto-target overtake velocities.
Other objects and many of the attendant advantages of this invention will become readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
FIG. 1 shows a schematic diagram of a preferred embodimcnt of the processing circuit.
FIG. 2 shows a modification of the circuit of FIG. 1.
FIG. 3 shows a further modification of the circuit of FIG. 1.
FIG. 4 shows graphically the point of firing of the circuit of FIG. 1.
Referring now to the drawings, wherein like reference characters designate like or corresponding parts throughout the several illustrations, there is shown in FIG. 1 the final amplifier stage 10- of an IR fuzing system (not shown) which provides the signal Wavefrom A; Because of the large modulation or'serrations present in Waveform A, a resistor-capacitor differentiating circuit would produce a premature pulse which would fire the fuze.
Waveform signal A is coupled through coupling capacitor 12 and diode 14 to charge capacitor 16 with a voltage as illustrated by Waveform C. Diode 14 is polarized so that a negative going signal is passed by the forward conductance of diode 14 but positive signals are blocked, thus, storing the negative peaks of Waveform A in capacitor 16. At the termination of the intercept Waveform A, the peak amplitude of the signal is stored in capacitor 16 and held by choosing the values of capacitor 16 and resistor 18 to have long time constant.
Waveform signal A is also coupled through coupling capacitor 20, with a small amount of integration as shown by Waveform B, and Zener Diode 22 to the control electrode of silicon controlled rectifier 24. As shown in FIG. 4, there is no voltage difference across Diode 22 so that it does not conduct. At the termination of the signal (Waveform A) as the IR source as seen by the IR detector passes from the detector field of view, Waveform B drops to zero, the voltage across Diode 22 increases until its breakdown voltage (V FIG. 4) is exceeded and it begins to conduct. This diode current is applied to the control electrode of controlled rectifier 24 and causes it to switch, thereby discharging capacitor 16 and producing a precise trigger pulse at terminal 28 to mark the termination of the detected signal. The portion 30 of Waveform C is the nor mal decay of resistor 18 and capacitor 16 time constant while the portion 32 shows the discharge when controlled rectifier 24 is switched on.
FIG. 2 is functionally the same as FIG. 1 but has been modified by replacing the dual coupling capacitors 12 and 20 with a single coupling capacitor 36.
FIG. 3 is functionally the same as FIG. 1 with the ad dition of diode 38 and integrating capacitor 40 to prevent narrow spikes from inadvertently firing rectifier 24.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. In a fuze processing circuit which is not influenced by a high degree of modulation present in the target envelope signal, the combination comprising:
a. a source of target envelope negative signals having a high degree of modulation,
b. a storage capacitor,
c. a diode coupling only the negative going portion and blocking the positive going portions of said target envelope signal to said storage capacitor,
d. an output terminal,
e. a normally non-conducting silicon controlled rectifier,
f. said silicon controlled rectifier being serially connected across said storage capacitor,
g. circuit means coupling the anode of said silicon controlled rectifier to said output terminal,
rectifier to a conducting condition to discharge said storage capacitor in response to the termination of a target envelope negative signal.

Claims (1)

1. In a fuze processing circuit which is not influenced by a high degree of modulation present in the target envelope signal, the combination comprising: a. a source of target envelope negative signals having a high degree of modulation, b. a storage Capacitor, c. a diode coupling only the negative going portion and blocking the positive going portions of said target envelope signal to said storage capacitor, d. an output terminal, e. a normally non-conducting silicon controlled rectifier, f. said silicon controlled rectifier being serially connected across said storage capacitor, g. circuit means coupling the anode of said silicon controlled rectifier to said output terminal, h. circuit means including a Zener diode coupled to said source of target envelope negative signals and to the control electrode of said normally non-conducting silicon controlled rectifier for switching said normally non-conducting silicon controlled rectifier to a conducting condition to discharge said storage capacitor in response to the termination of a target envelope negative signal.
US370740A 1964-05-27 1964-05-27 Fuze signal processing circuit Expired - Lifetime US3910192A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US370740A US3910192A (en) 1964-05-27 1964-05-27 Fuze signal processing circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US370740A US3910192A (en) 1964-05-27 1964-05-27 Fuze signal processing circuit

Publications (1)

Publication Number Publication Date
US3910192A true US3910192A (en) 1975-10-07

Family

ID=23460964

Family Applications (1)

Application Number Title Priority Date Filing Date
US370740A Expired - Lifetime US3910192A (en) 1964-05-27 1964-05-27 Fuze signal processing circuit

Country Status (1)

Country Link
US (1) US3910192A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1014029A3 (en) * 1998-12-22 2000-11-22 Diehl Munitionssysteme GmbH & Co. KG Detector circuit

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3022732A (en) * 1958-09-05 1962-02-27 Warren D Paley Thyratron firing circuit
US3173077A (en) * 1962-08-06 1965-03-09 Gen Motors Corp Semiconductor voltage regulator
US3198989A (en) * 1961-03-30 1965-08-03 American Mach & Foundry Electronic switch device with commutating capacitor
US3237023A (en) * 1961-12-29 1966-02-22 Bendix Corp Peak amplitude sensing circuit
US3236239A (en) * 1962-07-17 1966-02-22 American Optical Corp Defibrillator

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3022732A (en) * 1958-09-05 1962-02-27 Warren D Paley Thyratron firing circuit
US3198989A (en) * 1961-03-30 1965-08-03 American Mach & Foundry Electronic switch device with commutating capacitor
US3237023A (en) * 1961-12-29 1966-02-22 Bendix Corp Peak amplitude sensing circuit
US3236239A (en) * 1962-07-17 1966-02-22 American Optical Corp Defibrillator
US3173077A (en) * 1962-08-06 1965-03-09 Gen Motors Corp Semiconductor voltage regulator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1014029A3 (en) * 1998-12-22 2000-11-22 Diehl Munitionssysteme GmbH & Co. KG Detector circuit

Similar Documents

Publication Publication Date Title
US3316451A (en) Intervalometer
US4015530A (en) Two channel optical fuzing system
US3952660A (en) Fuze safing and arming device utilizing propellant ionization
US3980019A (en) Adaptive ordnance system
US3924233A (en) Active-passive target detection system
US4896606A (en) Optical proximity fuze
US4185560A (en) Fore and aft fuzing system
US3858207A (en) Range sensing target detecting device
EP1277024B1 (en) Electronic self-destruct device
US4939995A (en) Integrator and firing circuit for proximity fuzes
US3910192A (en) Fuze signal processing circuit
US3967557A (en) Adjustable electrical time delay fuze
US4972775A (en) Electrostatic passive proximity fuzing system
US2509910A (en) Time-delay circuit
US3166015A (en) Radio frequency proximity fuze
US4991508A (en) Electric field enabled proximity fuzing system
US4170008A (en) Clutter discriminating fuze apparatus
US3688701A (en) Command fuze
US3924536A (en) Fuze signal circuit
US3976012A (en) Arrangement for automatic switching in electric fuses for projectiles
US4382408A (en) Circuit arrangement for an impact fuze
US3908552A (en) Fuze signal processing circuit
US4185559A (en) Amplifier for missile detonator
US3889599A (en) Fuze
US2873679A (en) Ordnance fuze firing circuit