DE69632997D1 - Verfahren zur systematischen Kalibrierung von der vektoriellen Schubkraft für Momentumsregelung eines Satelliten - Google Patents

Verfahren zur systematischen Kalibrierung von der vektoriellen Schubkraft für Momentumsregelung eines Satelliten

Info

Publication number
DE69632997D1
DE69632997D1 DE69632997T DE69632997T DE69632997D1 DE 69632997 D1 DE69632997 D1 DE 69632997D1 DE 69632997 T DE69632997 T DE 69632997T DE 69632997 T DE69632997 T DE 69632997T DE 69632997 D1 DE69632997 D1 DE 69632997D1
Authority
DE
Germany
Prior art keywords
satellite
calibration method
momentum control
systematic calibration
vectorial
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
DE69632997T
Other languages
English (en)
Other versions
DE69632997T2 (de
Inventor
Michael F Barsky
Yocum, Jr
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 DE69632997D1 publication Critical patent/DE69632997D1/de
Application granted granted Critical
Publication of DE69632997T2 publication Critical patent/DE69632997T2/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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
DE69632997T 1995-12-22 1996-12-18 Verfahren zur systematischen Kalibrierung von der vektoriellen Schubkraft für Momentumsregelung eines Satelliten Expired - Lifetime DE69632997T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/577,595 US5765780A (en) 1995-12-22 1995-12-22 Systematic vectored thrust calibration method for satellite momentum control
US577595 1995-12-22

Publications (2)

Publication Number Publication Date
DE69632997D1 true DE69632997D1 (de) 2004-09-02
DE69632997T2 DE69632997T2 (de) 2005-07-21

Family

ID=24309397

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69632997T Expired - Lifetime DE69632997T2 (de) 1995-12-22 1996-12-18 Verfahren zur systematischen Kalibrierung von der vektoriellen Schubkraft für Momentumsregelung eines Satelliten

Country Status (3)

Country Link
US (1) US5765780A (de)
EP (1) EP0781706B1 (de)
DE (1) DE69632997T2 (de)

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US6042058A (en) * 1997-04-29 2000-03-28 Hughes Electronics Corporation Stationkeeping and momentum-dumping thruster systems and methods
US5944761A (en) * 1997-06-06 1999-08-31 Honeywell Inc. Variable periodic disturbance rejection filter
US6128556A (en) * 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
US6039290A (en) * 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
US6135394A (en) * 1998-12-08 2000-10-24 Space Systems/Loral, Inc. Practical method and apparatus for satellite stationkeeping
US6260805B1 (en) * 1998-12-29 2001-07-17 Hughes Electronics Corporation Method of controlling attitude of a momentum biased spacecraft during long-duration thruster firings
US6356814B1 (en) * 1999-02-03 2002-03-12 Microcosm, Inc. Spacecraft magnetic torquer feedback system
US6471161B1 (en) 1999-12-27 2002-10-29 Lockheed Martin Corporation Satellite attitude control system
US6254036B1 (en) * 2000-02-16 2001-07-03 Hughes Electronics Corporation Method and apparatus for spacecraft wheel desaturation
US6445981B1 (en) * 2000-03-02 2002-09-03 Space Systems/Loral, Inc. Controller and control method for satellite orbit-keeping maneuvers
US6481672B1 (en) * 2001-01-18 2002-11-19 Lockheed Martin Corporation Gimbaled thruster control system
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
US6637701B1 (en) 2002-04-03 2003-10-28 Lockheed Martin Corporation Gimbaled ion thruster arrangement for high efficiency stationkeeping
US6945500B2 (en) * 2003-08-15 2005-09-20 Skycorp, Inc. Apparatus for a geosynchronous life extension spacecraft
US7149610B2 (en) * 2003-08-26 2006-12-12 The Boeing Company Momentum estimator for on-station momentum control
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
CA2546201A1 (en) * 2006-05-08 2007-11-08 John B. Holland System and method for unloading angular momentum from a spacecraft momentum wheel stabilization system
DE102007002672B4 (de) * 2007-01-18 2023-08-10 Airbus Defence and Space GmbH Verfahren zur Ermittlung eines Flugzeugzustandes
US8352101B2 (en) * 2009-12-22 2013-01-08 The Boeing Company Algorithm for simultaneous attitude maneuver and momentum dumping
US8468794B1 (en) * 2010-01-15 2013-06-25 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Electric propulsion apparatus
US9180984B2 (en) * 2012-05-11 2015-11-10 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
US8915472B2 (en) * 2012-05-11 2014-12-23 The Boeing Company Multiple space vehicle launch system
CA2831309C (en) * 2012-12-04 2017-05-30 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
CN103235598B (zh) * 2013-05-14 2016-08-10 北京理工大学 一种调整推力器方向指向组合体航天器质心的方法
US20150001344A1 (en) * 2013-06-26 2015-01-01 Raytheon Company Satellite positioning system
RU2750349C2 (ru) 2014-08-26 2021-06-28 Астроскейл Израэл Лтд. Система и способ стыковки для спутников
US9764858B2 (en) * 2015-01-07 2017-09-19 Mitsubishi Electric Research Laboratories, Inc. Model predictive control of spacecraft
CN106586032B (zh) * 2016-11-14 2018-08-21 北京卫星环境工程研究所 航天器合舱状态设备安装精度的调整方法
CN106742072B (zh) * 2016-11-25 2019-07-12 深圳航天东方红海特卫星有限公司 一种高密度微小型一体化飞轮与磁力矩构型
US10625882B2 (en) * 2017-03-06 2020-04-21 Effective Space Solutions Ltd. Service satellite for providing in-orbit services using variable thruster control
CN111950074B (zh) * 2020-06-30 2024-02-09 中国空间技术研究院 一种确定并联贮箱航天器发射质心的方法及装置
CN112298614B (zh) * 2020-09-18 2021-09-14 中国人民解放军战略支援部队航天工程大学 一种推力在轨标定试验方法
CN112918705B (zh) * 2021-03-12 2022-07-12 深圳航天东方红卫星有限公司 一种一体化推进分系统的热控系统与方法
CN113218660B (zh) * 2021-06-14 2022-09-13 中国西安卫星测控中心 一种电推力矢量在轨标定方法

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US2963243A (en) * 1959-03-04 1960-12-06 Heinrich C Rothe Space vehicle guidance mechanism and method
US3907226A (en) * 1970-07-06 1975-09-23 Hughes Aircraft Co Redundant position and attitude control for spin stabilized devices
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
DE2539457C2 (de) * 1975-09-04 1982-07-01 RCA Corp., 10020 New York, N.Y. Verfahren und Steuersystem zum Eliminieren der Nutation eines Raumflugkörpers
US4230294A (en) * 1979-07-23 1980-10-28 Rca Corporation Closed loop roll control for momentum biased satellites
EP0046151B1 (de) * 1980-08-19 1985-11-21 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Vorrichtung zur Lagestabilisierung von elastischen Fahrzeugen
FR2656586B1 (fr) * 1989-12-29 1992-05-07 Aerospatiale Dispositif de controle d'attitude par voiles solaires pour satellite stabilise autour de trois axes.
IT1245661B (it) * 1991-01-23 1994-10-06 Selenia Spazio Spa Ora Alenia Satellite stabilizzato a tre assi dotato di propulsori elettrici per manovre orbitali e controllo di assetto.
CA2080612A1 (en) * 1991-11-27 1993-05-28 Douglas J. Bender Method and apparatus for compensating for magnetic disturbance torques on a satellite
US5337981A (en) * 1991-11-27 1994-08-16 Hughes Aircraft Company Method and apparatus for compensating for solar torque transients on a satellite during a solar eclipse
US5349532A (en) * 1992-04-28 1994-09-20 Space Systems/Loral Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters
US5308024A (en) * 1992-07-20 1994-05-03 General Electric Co. Disturbance torque compensated three axis yaw control system
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
US5443231A (en) * 1993-11-17 1995-08-22 Hughes Aircraft Company Method and apparatus for a satellite station keeping
US5571953A (en) * 1995-05-15 1996-11-05 The Boeing Company Method and apparatus for the linear real time estimation of an aircraft center of gravity

Also Published As

Publication number Publication date
EP0781706A2 (de) 1997-07-02
EP0781706A3 (de) 1997-12-03
DE69632997T2 (de) 2005-07-21
EP0781706B1 (de) 2004-07-28
US5765780A (en) 1998-06-16

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Legal Events

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8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART