DE69707327D1 - Einachsige Korrektur für Bahnneigung - Google Patents

Einachsige Korrektur für Bahnneigung

Info

Publication number
DE69707327D1
DE69707327D1 DE69707327T DE69707327T DE69707327D1 DE 69707327 D1 DE69707327 D1 DE 69707327D1 DE 69707327 T DE69707327 T DE 69707327T DE 69707327 T DE69707327 T DE 69707327T DE 69707327 D1 DE69707327 D1 DE 69707327D1
Authority
DE
Germany
Prior art keywords
web inclination
uniaxial
correction
uniaxial correction
inclination
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
DE69707327T
Other languages
English (en)
Other versions
DE69707327T2 (de
Inventor
Richard A Fowell
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Publication of DE69707327D1 publication Critical patent/DE69707327D1/de
Application granted granted Critical
Publication of DE69707327T2 publication Critical patent/DE69707327T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
DE69707327T 1996-02-28 1997-02-19 Einachsige Korrektur für Bahnneigung Expired - Lifetime DE69707327T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/608,238 US5738309A (en) 1996-02-28 1996-02-28 Single axis correction for orbit inclination

Publications (2)

Publication Number Publication Date
DE69707327D1 true DE69707327D1 (de) 2001-11-22
DE69707327T2 DE69707327T2 (de) 2002-06-27

Family

ID=24435630

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69707327T Expired - Lifetime DE69707327T2 (de) 1996-02-28 1997-02-19 Einachsige Korrektur für Bahnneigung

Country Status (4)

Country Link
US (1) US5738309A (de)
EP (1) EP0792800B1 (de)
JP (1) JP3782193B2 (de)
DE (1) DE69707327T2 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5911389A (en) * 1996-12-20 1999-06-15 Lockheed Martin Corp. Wave based satellite constellation
US6108593A (en) * 1997-07-09 2000-08-22 Hughes Electronics Corporation Method and apparatus for estimating attitude sensor bias in a satellite
US6154692A (en) * 1997-10-01 2000-11-28 Space Systems/Loral, Inc. Spacecraft yaw pointing for inclined orbits
US7198230B2 (en) * 1997-10-14 2007-04-03 The Directv Group, Inc. Method and system for maximizing satellite constellation coverage
US6081227A (en) * 1998-01-05 2000-06-27 Motorola, Inc. Method and apparatus for beam management in a satellite communication system
DE19847480A1 (de) * 1998-10-15 2000-04-27 Daimler Chrysler Ag Verfahren und Vorrichtung zur Lagebestimmung von Kommunikations-Satelliten
US6257526B1 (en) * 1998-11-09 2001-07-10 Hughes Electronics Corporation Satellite system and method of deploying same
US6152403A (en) * 1998-11-11 2000-11-28 Hughes Electronics Corporation Gyroscopic calibration methods for spacecraft
US6327523B2 (en) 1999-01-21 2001-12-04 Hughes Electronics Corporation Overhead system of inclined eccentric geosynchronous orbitting satellites
US6318676B1 (en) * 2000-01-10 2001-11-20 Space Systems/Loral, Inc. Equatorial-normal body-stabilized spacecraft and control method for inclined orbit operation
US7184761B1 (en) * 2000-03-27 2007-02-27 The Directv Group, Inc. Satellite communications system
US7369809B1 (en) 2000-10-30 2008-05-06 The Directv Group, Inc. System and method for continuous broadcast service from non-geostationary orbits
US6732977B1 (en) * 2002-02-11 2004-05-11 Lockheed Martin Corporation System for on-orbit correction of spacecraft payload pointing errors
US6695263B1 (en) 2002-02-12 2004-02-24 Lockheed Martin Corporation System for geosynchronous spacecraft rapid earth reacquisition
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6702234B1 (en) 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US6892987B2 (en) * 2003-07-25 2005-05-17 Sirius Satellite Radio Inc. Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
US8205839B2 (en) * 2006-11-06 2012-06-26 The Boeing Company Methods and apparatus for node-synchronous eccentricity control
FR2929782B1 (fr) * 2008-04-07 2010-06-04 Centre Nat Etd Spatiales Satellite agile a antennes de transmission reparties
US8589015B2 (en) * 2010-02-12 2013-11-19 Webtech Wireless Inc. Vehicle sensor calibration for determining vehicle dynamics
IL207536A (en) * 2010-08-11 2016-11-30 Israel Aerospace Ind Ltd A system and method for measuring aviation platform angular orientation
US9114893B2 (en) * 2012-07-26 2015-08-25 Mitsubishi Electric Research Laboratories, Inc. System and method for estimating states of spacecraft in planet-moon environment
KR101782259B1 (ko) * 2016-04-21 2017-09-27 한국항공우주연구원 위성 안테나 속도 제어 장치 및 방법
US10392136B2 (en) * 2017-09-18 2019-08-27 Raytheon Company Offload adjustment for satellite image diversity

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3866025A (en) * 1972-03-17 1975-02-11 Rca Corp Spacecraft attitude control system
US4084772A (en) * 1976-01-28 1978-04-18 Rca Corporation Roll/yaw body steering for momentum biased spacecraft
US4294420A (en) * 1978-01-30 1981-10-13 Matra Attitude control systems for space vehicles
FR2580582B1 (fr) * 1985-04-19 1987-06-26 Matra Procede et dispositif d'amortissement de nutation de satellite par commande d'orientation de masses presentant un produit d'inertie variable
JP2635564B2 (ja) * 1985-07-18 1997-07-30 ヒユ−ズ・エアクラフト・カンパニ− 自転している宇宙船用の自律性の回転軸姿勢制御方法
US4757964A (en) * 1986-07-17 1988-07-19 Hughes Aircraft Company Method for controlling the attitude of a spinning body in orbit
US4776540A (en) * 1986-10-03 1988-10-11 Communications Satellite Corporation Method of orienting a synchronous satellite
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
JPH02274697A (ja) * 1989-04-14 1990-11-08 Toshiba Corp 宇宙航行体の姿勢制御装置
DE3922761C2 (de) * 1989-07-11 1994-08-25 Deutsche Aerospace Verfahren und Vorrichtung zum Ausrichten eines geostationären Satelliten in einer Referenzrichtung
FR2655167B1 (fr) * 1989-11-29 1992-04-03 Aerospatiale Procede de controle d'attitude en roulis et en lacet d'un satellite.
US5100084A (en) * 1990-04-16 1992-03-31 Space Systems/Loral, Inc. Method and apparatus for inclined orbit attitude control for momentum bias spacecraft
US5184790A (en) * 1991-07-22 1993-02-09 Hughes Aircraft Company Two-axis attitude correction for orbit inclination
US5257760A (en) * 1992-06-24 1993-11-02 Edo Corporation, Barnes Engineering Division Scanning earth sensor using the sun's position for determining yaw
US5437420A (en) * 1993-07-16 1995-08-01 Hughes Aircraft Company High torque double gimbal control moment gyro
US5443231A (en) * 1993-11-17 1995-08-22 Hughes Aircraft Company Method and apparatus for a satellite station keeping
US5476239A (en) * 1994-04-19 1995-12-19 The United States Of America As Represented By The Secretary Of The Navy Gyro platform assembly with a spinning vehicle

Also Published As

Publication number Publication date
US5738309A (en) 1998-04-14
JP3782193B2 (ja) 2006-06-07
JPH09328100A (ja) 1997-12-22
EP0792800B1 (de) 2001-10-17
DE69707327T2 (de) 2002-06-27
EP0792800A1 (de) 1997-09-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition