DE69131405D1 - Methode zur Steuerung der Lage eines durch Eigenrotation stabilisierten Satelliten in einer geneigten Umlaufbahn - Google Patents

Methode zur Steuerung der Lage eines durch Eigenrotation stabilisierten Satelliten in einer geneigten Umlaufbahn

Info

Publication number
DE69131405D1
DE69131405D1 DE69131405T DE69131405T DE69131405D1 DE 69131405 D1 DE69131405 D1 DE 69131405D1 DE 69131405 T DE69131405 T DE 69131405T DE 69131405 T DE69131405 T DE 69131405T DE 69131405 D1 DE69131405 D1 DE 69131405D1
Authority
DE
Germany
Prior art keywords
self
controlling
rotation
inclined orbit
satellite stabilized
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 - Fee Related
Application number
DE69131405T
Other languages
English (en)
Other versions
DE69131405T2 (de
Inventor
Christopher D Rahn
John A Lehner
Donald W Gamble
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.)
Maxar Space LLC
Original Assignee
Space Systems Loral LLC
Loral Space Systems 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 Space Systems Loral LLC, Loral Space Systems Inc filed Critical Space Systems Loral LLC
Application granted granted Critical
Publication of DE69131405D1 publication Critical patent/DE69131405D1/de
Publication of DE69131405T2 publication Critical patent/DE69131405T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • 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
    • 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
    • B64G1/26—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
    • 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
    • B64G1/28—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
DE69131405T 1990-04-16 1991-03-19 Methode zur Steuerung der Lage eines durch Eigenrotation stabilisierten Satelliten in einer geneigten Umlaufbahn Expired - Fee Related DE69131405T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US51032190A 1990-04-16 1990-04-16
US07/579,117 US5100084A (en) 1990-04-16 1990-09-07 Method and apparatus for inclined orbit attitude control for momentum bias spacecraft

Publications (2)

Publication Number Publication Date
DE69131405D1 true DE69131405D1 (de) 1999-08-05
DE69131405T2 DE69131405T2 (de) 1999-12-16

Family

ID=27056865

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69131405T Expired - Fee Related DE69131405T2 (de) 1990-04-16 1991-03-19 Methode zur Steuerung der Lage eines durch Eigenrotation stabilisierten Satelliten in einer geneigten Umlaufbahn
DE69126233T Expired - Fee Related DE69126233T2 (de) 1990-04-16 1991-03-19 Vorrichtung zur Steuerung der Lage eines Satelliten in einer geneigten Umlaufbahn

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE69126233T Expired - Fee Related DE69126233T2 (de) 1990-04-16 1991-03-19 Vorrichtung zur Steuerung der Lage eines Satelliten in einer geneigten Umlaufbahn

Country Status (5)

Country Link
US (1) US5100084A (de)
EP (3) EP0769736B1 (de)
JP (1) JP3244717B2 (de)
CA (1) CA2040590C (de)
DE (2) DE69131405T2 (de)

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US5787368A (en) * 1995-11-03 1998-07-28 Space Systems/Loral, Inc. Spacecraft yaw control using only wheel speed measurements processed through a simple filter bank
US5791598A (en) * 1996-01-16 1998-08-11 Globalstar L.P. and Daimler-Benz Aerospace AG Dynamic bias for orbital yaw steering
US5738309A (en) * 1996-02-28 1998-04-14 Hughes Electronics Single axis correction for orbit inclination
US5992799A (en) * 1996-03-08 1999-11-30 Space Systems/Loral, Inc. Earth based spacecraft orbit and attitude control using a look-ahead thruster selection logic and magnetic torquers
US6047226A (en) * 1997-06-26 2000-04-04 Hughes Electronics Corporation Enhanced stellar attitude determination system
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
US6047927A (en) * 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control
US6135389A (en) * 1998-03-16 2000-10-24 Hughes Electronics Corporation Subterranean target steering strategy
US6288670B1 (en) * 1999-12-23 2001-09-11 Hughes Electronics Corporation Combined roll-yaw spacecraft steering method for low earth orbit target trajectory compensation
US6292722B1 (en) * 2000-02-24 2001-09-18 Space Systems/Loral, Inc. Magnetic torquer control with thruster augmentation
US6535734B1 (en) * 2000-04-04 2003-03-18 Motorola, Inc. Method and apparatus for steering mobile platform beams
US6470243B1 (en) 2000-06-30 2002-10-22 Hughes Electronics Corp. Correction of spacecraft steering control law for unexpected orbital inclination effects
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
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
KR100793058B1 (ko) 2006-09-27 2008-01-10 한국전자통신연구원 지향 목표 궤적 근사화를 이용한 위성 자세 제어 방법
US8205839B2 (en) * 2006-11-06 2012-06-26 The Boeing Company Methods and apparatus for node-synchronous eccentricity control
US9045239B2 (en) * 2009-01-14 2015-06-02 Space Systems/Loral, Llc Spacecraft payload orientation steering
US8174433B1 (en) 2009-02-26 2012-05-08 Raytheon Company Bias estimation and orbit determination
US20110260006A1 (en) * 2010-01-11 2011-10-27 Cyrus Mohammad Ali Nejat Nejat kinematics and kinetics expansions spacecraft
US8915472B2 (en) 2012-05-11 2014-12-23 The Boeing Company Multiple space vehicle launch system
US9180984B2 (en) 2012-05-11 2015-11-10 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
CA2831309C (en) * 2012-12-04 2017-05-30 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
CN104252546A (zh) * 2013-06-26 2014-12-31 上海新跃仪表厂 一种火星捕获制动参数优化方法
FR3033056B1 (fr) * 2015-02-25 2019-05-03 Centre National D'etudes Spatiales (Cnes) Procede de determination des parametres de guidage d'un satellite pour suivre une trajectoire
CN105138010B (zh) * 2015-08-31 2017-07-28 哈尔滨工业大学 一种编队卫星分布式有限时间跟踪控制方法
US9641280B1 (en) * 2015-12-10 2017-05-02 Intelligent Fusion Technology, Inc Anti-jamming method in satellite communication (SATCOM) system
CN109032176B (zh) * 2018-07-25 2021-06-22 西北工业大学 一种基于微分代数的地球同步轨道确定和参数确定方法
CN109159923B (zh) * 2018-07-26 2022-05-13 西北工业大学 一种航天器追踪目标丢失段的相对可达区域计算方法
US11279501B2 (en) * 2018-10-25 2022-03-22 General Atomics Satellite attitude control system using eigen vector, non-linear dynamic inversion, and feedforward control
CN109573105B (zh) * 2018-11-19 2022-06-14 上海埃依斯航天科技有限公司 末子级留轨应用子系统姿态控制方法
CN110104217A (zh) * 2019-03-29 2019-08-09 上海卫星工程研究所 卫星姿态控制与大角动量补偿复用飞轮的构形与控制方法
CN110329548B (zh) * 2019-05-24 2023-01-17 中国人民解放军63789部队 航天器在轨转偏置控制下飞轮系统重构方法
CN111121765B (zh) * 2019-12-16 2021-09-24 上海航天控制技术研究所 共用遥感卫星平台的对地灵巧观测与对天geo目标监视方法
CN111399531B (zh) * 2020-04-23 2023-04-07 中国人民解放军国防科技大学 高超声速飞行器滑翔段制导与姿态控制一体化设计方法
CN113238572B (zh) * 2021-05-31 2022-11-22 上海海事大学 基于预设性能控制的预设时间四旋翼无人机姿态跟踪方法
CN113401365B (zh) * 2021-06-15 2022-05-24 北京控制工程研究所 倾斜轨道海洋动力卫星高精度轨控过程中的能源控制方法
CN114735239B (zh) * 2022-04-27 2022-10-18 中国人民解放军32039部队 航天器轨道机动控制方法、装置和电子设备
CN116750211B (zh) * 2023-07-13 2024-01-23 四川大学 一种基于追踪目标分配与轨道规划的追踪防御方法

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Also Published As

Publication number Publication date
JPH0789499A (ja) 1995-04-04
EP0453096A1 (de) 1991-10-23
EP0769736A1 (de) 1997-04-23
DE69126233D1 (de) 1997-07-03
EP0769736B1 (de) 1999-06-30
EP0628899A1 (de) 1994-12-14
CA2040590C (en) 1999-07-27
DE69131405T2 (de) 1999-12-16
CA2040590A1 (en) 1991-10-17
JP3244717B2 (ja) 2002-01-07
US5100084A (en) 1992-03-31
DE69126233T2 (de) 1997-11-27
EP0453096B1 (de) 1997-05-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee