DE69108215T2 - System zur Lagestabilisierung eines dreiachsenstabilisierten Satelliten auf einer Umlaufbahn mit kleiner Bahnneigung. - Google Patents

System zur Lagestabilisierung eines dreiachsenstabilisierten Satelliten auf einer Umlaufbahn mit kleiner Bahnneigung.

Info

Publication number
DE69108215T2
DE69108215T2 DE69108215T DE69108215T DE69108215T2 DE 69108215 T2 DE69108215 T2 DE 69108215T2 DE 69108215 T DE69108215 T DE 69108215T DE 69108215 T DE69108215 T DE 69108215T DE 69108215 T2 DE69108215 T2 DE 69108215T2
Authority
DE
Germany
Prior art keywords
orbit
stabilizing
small
axis stabilized
stabilized satellite
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
DE69108215T
Other languages
English (en)
Other versions
DE69108215D1 (de
Inventor
Issam Maurice Achkar
Pierre Guillermin
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69108215D1 publication Critical patent/DE69108215D1/de
Application granted granted Critical
Publication of DE69108215T2 publication Critical patent/DE69108215T2/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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star 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
    • B64G1/36—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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth 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
    • B64G1/28—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
DE69108215T 1990-12-21 1991-12-20 System zur Lagestabilisierung eines dreiachsenstabilisierten Satelliten auf einer Umlaufbahn mit kleiner Bahnneigung. Expired - Fee Related DE69108215T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9016149A FR2670745B1 (fr) 1990-12-21 1990-12-21 Systeme de controle d'attitude pour satellite stabilise 3-axes sur orbite a faible inclinaison.

Publications (2)

Publication Number Publication Date
DE69108215D1 DE69108215D1 (de) 1995-04-20
DE69108215T2 true DE69108215T2 (de) 1995-11-16

Family

ID=9403571

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69108215T Expired - Fee Related DE69108215T2 (de) 1990-12-21 1991-12-20 System zur Lagestabilisierung eines dreiachsenstabilisierten Satelliten auf einer Umlaufbahn mit kleiner Bahnneigung.

Country Status (6)

Country Link
US (1) US5259577A (de)
EP (1) EP0493227B1 (de)
JP (1) JPH04308906A (de)
CA (1) CA2057720A1 (de)
DE (1) DE69108215T2 (de)
FR (1) FR2670745B1 (de)

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FR2691426B1 (fr) * 1992-05-19 1997-09-19 Aerospatiale Procede et dispositif d'acquisition de la terre via la polaire pour satellite stabilise 3-axes en orbite de faible inclinaison.
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US5354016A (en) * 1992-07-30 1994-10-11 General Electric Co. Pivoted wheel roll control with automatic offset
RU2033949C1 (ru) * 1993-02-09 1995-04-30 Севастиян Дмитриевич Гнатюк Автономная бортовая система управления космического аппарата "гасад"
US5412574A (en) * 1993-05-14 1995-05-02 Hughes Aircraft Company Method of attitude determination using earth and star sensors
US5437420A (en) * 1993-07-16 1995-08-01 Hughes Aircraft Company High torque double gimbal control moment gyro
DE19510371C1 (de) * 1995-03-22 1996-10-31 Daimler Benz Aerospace Ag Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit
DE19518617A1 (de) * 1995-05-24 1996-11-28 Daimler Benz Aerospace Ag Dreiachsenstabilisierter, erdorientierter Satellit und zugehöriges Sonnen- und Erdakquisitonsverfahren unter Benutzung eines Magnetometers
DE19520410A1 (de) * 1995-06-09 1996-12-12 Daimler Benz Aerospace Ag Erdorientierter Satellit und Verfahren zur Lage-, Nutations- und Raddrallregelung
AU7118896A (en) * 1995-09-28 1997-04-17 Lockheed Martin Corporation Techniques for optimizing an autonomous star tracker
US5791598A (en) * 1996-01-16 1998-08-11 Globalstar L.P. and Daimler-Benz Aerospace AG Dynamic bias for orbital yaw steering
US5852792A (en) * 1996-10-03 1998-12-22 Lockheed Martin Corporation Spacecraft boresight calibration filter
US5935176A (en) * 1996-11-22 1999-08-10 Lockheed Martin Corporation Momentum wheel oscillation filter
US6047226A (en) * 1997-06-26 2000-04-04 Hughes Electronics Corporation Enhanced stellar attitude determination system
JP3483746B2 (ja) * 1997-11-14 2004-01-06 宇宙開発事業団 西回り赤道周回衛星及び該衛星を用いた気象衛星システム
US6298288B1 (en) * 1998-12-16 2001-10-02 Hughes Electronics Corp. Autonomous gyro scale factor and misalignment calibration
US6020956A (en) * 1999-02-04 2000-02-01 The Aerospace Corporation Pseudo gyro
US6471161B1 (en) * 1999-12-27 2002-10-29 Lockheed Martin Corporation Satellite attitude control system
US6292722B1 (en) * 2000-02-24 2001-09-18 Space Systems/Loral, Inc. Magnetic torquer control with thruster augmentation
US6253125B1 (en) * 2000-03-01 2001-06-26 Space Systems/Loral, Inc. Method and apparatus for generating orbital data
US6263264B1 (en) * 2000-06-08 2001-07-17 The Aerospace Corporation Pseudo gyro with unmodeled disturbance torque estimation
JP3859454B2 (ja) * 2001-03-01 2006-12-20 Ｎｅｃ東芝スペースシステム株式会社 人工衛星のマヌーバ制御装置
FR2875354B1 (fr) * 2004-09-13 2006-12-22 Eads Astrium Sas Soc Par Actio Procede de transmission optique entre un terminal embarque sur un engin spatial et un terminal distant, et engin spatial adapte pour un tel procede
CN100451898C (zh) * 2005-12-14 2009-01-14 上海微小卫星工程中心 微小卫星的姿态控制方法及系统
US7692584B2 (en) * 2007-01-31 2010-04-06 Nd Satcom Gmbh Antenna system driven by intelligent components communicating via data-bus, and method and computer program therefore
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
US8380370B2 (en) * 2009-02-03 2013-02-19 The Boeing Company Spacecraft acquisition maneuvers using position-based gyroless control
US20130133445A1 (en) * 2011-11-29 2013-05-30 Christopher Jan Heiberg Control moment gyroscope desaturation in aircraft
DE102012222884A1 (de) * 2012-12-12 2014-06-12 Robert Bosch Gmbh Verfahren zur Stabilisierung eines Zweirads
US9073648B2 (en) * 2013-02-15 2015-07-07 The Boeing Company Star tracker rate estimation with kalman filter enhancement
US9296496B2 (en) * 2013-03-04 2016-03-29 Raytheon Company Thermal management system and method for space and air-borne sensors
CN103455035B (zh) * 2013-08-26 2015-12-23 北京理工大学 基于反步设计和非线性反馈的pd+姿态控制律设计方法
CN104071355B (zh) * 2014-06-12 2016-03-30 上海微小卫星工程中心 一种卫星姿态稳定控制方法及装置
FR3026858B1 (fr) * 2014-10-02 2016-12-09 Airbus Defence & Space Sas Procede de controle d'attitude d'un satellite en mode survie, satellite adapte et procede de commande a distance d'un tel satellite
RU2610793C1 (ru) * 2016-01-13 2017-02-15 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт химии и механики" (ФГУП ЦНИИХМ) Способ управления космическим аппаратом, снабженным многосопловой двигательной установкой
US9714101B1 (en) * 2016-10-25 2017-07-25 Marshall H. Kaplan Apparatus and methods for orbital debris removal
FR3058393A1 (fr) * 2016-11-10 2018-05-11 Airbus Defence And Space Sas Engin spatial comprenant des moyens de controle actif d’attitude et des moyens de controle passif d’attitude
KR101898641B1 (ko) * 2017-08-16 2018-10-31 한국항공우주연구원 인공위성 및 이의 제어 방법
US10059470B1 (en) 2018-02-09 2018-08-28 Launchspace Technologies Corporation Apparatus and methods for creating artificial geosynchronous orbits
US10543939B2 (en) 2018-02-09 2020-01-28 Launchspace Technologies Corporation Apparatus and methods for creating artificial near-earth orbits
CN108983801B (zh) * 2018-08-14 2021-05-28 北京航空航天大学 一种基于反作用飞轮动态特性的航天器抗干扰姿控方法
CN109677638B (zh) * 2019-01-30 2020-09-01 上海微小卫星工程中心 一种基于地磁场测量参数的改进的纯磁控自旋对日定向方法
FR3110144A1 (fr) * 2020-05-12 2021-11-19 Airbus Defence And Space Sas Procédé de contrôle d’orbite et de désaturation d’un satellite au moyen d’un unique bras articulé portant une unité de propulsion

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US4010921A (en) * 1975-08-20 1977-03-08 The United States Of America As Represented By The Secretary Of The Air Force Spacecraft closed loop three-axis momentum unloading system
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4114841A (en) * 1977-02-22 1978-09-19 Rca Corporation Magnetic torquing system for changing the spin rate of an orbiting satellite
US4521855A (en) * 1981-07-27 1985-06-04 Ford Aerospace & Communications Corporation Electronic on-orbit roll/yaw satellite control
DE3214373A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und einrichtung fuer die lageregelung eines satelliten
FR2655167B1 (fr) * 1989-11-29 1992-04-03 Aerospatiale Procede de controle d'attitude en roulis et en lacet d'un satellite.

Also Published As

Publication number Publication date
FR2670745A1 (fr) 1992-06-26
US5259577A (en) 1993-11-09
DE69108215D1 (de) 1995-04-20
FR2670745B1 (fr) 1993-04-16
CA2057720A1 (fr) 1992-06-22
EP0493227B1 (de) 1995-03-15
EP0493227A1 (de) 1992-07-01
JPH04308906A (ja) 1992-10-30

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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