DE69107043D1 - System zur Lagestabilisierung eines dreiachs-stabilisierten Satelliten, insbesondere eines Beobachtungssatelliten. - Google Patents

System zur Lagestabilisierung eines dreiachs-stabilisierten Satelliten, insbesondere eines Beobachtungssatelliten.

Info

Publication number
DE69107043D1
DE69107043D1 DE69107043T DE69107043T DE69107043D1 DE 69107043 D1 DE69107043 D1 DE 69107043D1 DE 69107043 T DE69107043 T DE 69107043T DE 69107043 T DE69107043 T DE 69107043T DE 69107043 D1 DE69107043 D1 DE 69107043D1
Authority
DE
Germany
Prior art keywords
satellite
stabilizing
observation
triaxially
triaxially 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
DE69107043T
Other languages
English (en)
Other versions
DE69107043T2 (de
Inventor
Bernard Blancke
Marc Attanasio
Patrick Maute
Issam-Maurice Achkar
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
Application granted granted Critical
Publication of DE69107043D1 publication Critical patent/DE69107043D1/de
Publication of DE69107043T2 publication Critical patent/DE69107043T2/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
    • B64G1/365—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
    • B64G1/244—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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69107043T 1990-12-21 1991-11-20 System zur Lagestabilisierung eines dreiachs-stabilisierten Satelliten, insbesondere eines Beobachtungssatelliten. Expired - Fee Related DE69107043T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9016150A FR2670746B1 (fr) 1990-12-21 1990-12-21 Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.

Publications (2)

Publication Number Publication Date
DE69107043D1 true DE69107043D1 (de) 1995-03-09
DE69107043T2 DE69107043T2 (de) 1995-05-24

Family

ID=9403573

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69107043T Expired - Fee Related DE69107043T2 (de) 1990-12-21 1991-11-20 System zur Lagestabilisierung eines dreiachs-stabilisierten Satelliten, insbesondere eines Beobachtungssatelliten.

Country Status (6)

Country Link
US (1) US5279483A (de)
EP (1) EP0493143B1 (de)
JP (1) JPH04293698A (de)
CA (1) CA2057804A1 (de)
DE (1) DE69107043T2 (de)
FR (1) FR2670746B1 (de)

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US5562266A (en) * 1992-10-29 1996-10-08 Aerospatiale Societe Nationale Industrielle Rate gyro calibration method and apparatus for a three-axis stabilized satellite
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DE19510371C1 (de) * 1995-03-22 1996-10-31 Daimler Benz Aerospace Ag Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit
US5667171A (en) * 1995-04-28 1997-09-16 Hughes Aircraft Company Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device
DE19518617A1 (de) * 1995-05-24 1996-11-28 Daimler Benz Aerospace Ag Dreiachsenstabilisierter, erdorientierter Satellit und zugehöriges Sonnen- und Erdakquisitonsverfahren unter Benutzung eines Magnetometers
US5788189A (en) * 1995-06-15 1998-08-04 Nec Corporation Spacecraft and an attitude control method for a spacecraft
EP0795806B1 (de) * 1995-08-11 2001-12-05 Astrium GmbH Vorrichtung zur Lageregelung und Stabilisierung eines Raumfahrzeuges
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
US5826829A (en) * 1996-07-15 1998-10-27 Space Systems/Loral Inc. Spacecraft control system with a trihedral momentum bias wheel configuration
JP3034807B2 (ja) * 1996-08-30 2000-04-17 三菱電機株式会社 人工衛星の姿勢決定装置
US5963862A (en) * 1996-10-25 1999-10-05 Pt Pasifik Satelit Nusantara Integrated telecommunications system providing fixed and mobile satellite-based services
US6067453A (en) * 1996-10-25 2000-05-23 Pt Pasifik Satelit Nusantara Satellite-based direct access telecommunications systems
US5921505A (en) * 1996-12-02 1999-07-13 Trw Inc. System and method for reducing mechanical disturbances from energy storage flywheels
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
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels
US6138953A (en) * 1998-03-02 2000-10-31 Hughes Electronics Corporation Slew rate direction determination for acquisition maneuvers using reaction wheels
US6340137B1 (en) * 1998-08-26 2002-01-22 Honeywell International Inc. Moment control unit for spacecraft attitude control
US6296207B1 (en) * 1999-01-27 2001-10-02 Space Systems/Loral, Inc. Combined stationkeeping and momentum management
US6285928B1 (en) * 2000-01-06 2001-09-04 Space Systems/Loral, Inc. Onboard attitude control using reaction wheels
US6456907B1 (en) * 2000-01-31 2002-09-24 Space Systems/Loral, Inc. System and method for limiting the effects of actuator saturation to certain body axes of a spacecraft
US6550721B2 (en) * 2000-03-09 2003-04-22 The Boeing Company Safing mode for high momentum states in body stabilized spacecraft
FR2821683B1 (fr) * 2001-03-01 2003-06-13 Agence Spatiale Europeenne Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace
US6691955B2 (en) * 2001-11-27 2004-02-17 Space Systems/Loral Spacecraft having a momentum wheel configuration that prevents zero wheel speeds
US6758444B1 (en) * 2002-12-30 2004-07-06 Honeywell International Inc. Momentum control system and method
US6845952B2 (en) * 2003-01-10 2005-01-25 Honeywell International, Inc. Flywheel prognostic health and fault management system and method
DE10342866A1 (de) * 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung
FR2870609B1 (fr) * 2004-05-18 2006-08-18 Alcatel Sa Dispositif electromagnetique de generation d'une force et d'un couple en vue du positionnement d'un corps
EA201101043A1 (ru) * 2010-07-15 2012-06-29 Руслан Николаевич Дейкарханов Способ дейкарханова трехмерного движения
CN102001453B (zh) * 2010-10-27 2013-01-23 北京控制工程研究所 一种增加前馈补偿改善磁控能力的方法
US20120160965A1 (en) * 2010-12-23 2012-06-28 Muller Ronald M Method to achieve a rapid and low power slew of a satellite
CN102229362B (zh) * 2011-04-29 2013-05-01 航天东方红卫星有限公司 敏捷卫星成像反向推扫速度失配时的姿态补偿方法
CN102436262B (zh) * 2011-09-26 2013-12-04 北京航空航天大学 高精度大负载航空遥感三轴惯性稳定平台控制系统及方法
US9334068B2 (en) * 2014-04-04 2016-05-10 NOA Inc. Unified orbit and attitude control for nanosatellites using pulsed ablative thrusters
CN103941740B (zh) * 2014-04-15 2016-07-06 北京控制工程研究所 一种考虑地球椭率的多轴机动成像卫星偏航姿态控制方法
CN104848859B (zh) * 2014-12-26 2016-06-01 北京航天控制仪器研究所 一种三轴惯性稳定平台及其自定位定向的控制方法
US10005568B2 (en) 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
FR3050982B1 (fr) * 2016-05-03 2018-06-15 Centre National D'etudes Spatiales (Cnes) Module de pilotage de desaturation des roues, dispositif de controle d'attitude d'un engin spatial et procede de desaturation des roues associe
US9921099B1 (en) * 2016-09-01 2018-03-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Spherical occulter coronagraph cubesat
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
CN107933968B (zh) * 2017-11-14 2019-06-18 中国运载火箭技术研究院 一种三飞轮一体化布局装置及其安装调整方法
FR3093326B1 (fr) * 2019-03-01 2024-10-04 Centre Nat Detudes Spatiales Procédé de contrôle de l’attitude d’un satellite en orbite basse
FR3093998B1 (fr) * 2019-03-20 2021-09-10 Airbus Defence & Space Sas Procédé de contrôle d’attitude d’un satellite en mode survie sans connaissance a priori de l’heure locale de l’orbite du satellite
CN112228250B (zh) * 2020-09-10 2023-06-09 沈阳航天新光集团有限公司 一种液体姿控发动机集成块
CN112960145B (zh) * 2021-02-04 2022-12-13 上海卫星工程研究所 一种遥感卫星对地姿态机动扫描的轨迹规划方法及系统
CN113619816B (zh) * 2021-09-06 2023-06-09 中国科学院微小卫星创新研究院 一种用于卫星的模块化姿控单元
CN115027702B (zh) * 2022-07-20 2023-05-05 南京理工大学 一种立方星零动量姿态控制系统结构的设计方法
CN115384811B (zh) * 2022-09-06 2024-05-14 北京控制工程研究所 V型轮控且单轮掉电卫星的三轴姿态快速稳定控制方法

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Also Published As

Publication number Publication date
CA2057804A1 (fr) 1992-06-22
FR2670746B1 (fr) 1993-04-16
EP0493143B1 (de) 1995-01-25
DE69107043T2 (de) 1995-05-24
US5279483A (en) 1994-01-18
JPH04293698A (ja) 1992-10-19
EP0493143A1 (de) 1992-07-01
FR2670746A1 (fr) 1992-06-26

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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