FR2659061B1 - Procede de stabilisation d'un satellite. - Google Patents

Procede de stabilisation d'un satellite.

Info

Publication number
FR2659061B1
FR2659061B1 FR909013193A FR9013193A FR2659061B1 FR 2659061 B1 FR2659061 B1 FR 2659061B1 FR 909013193 A FR909013193 A FR 909013193A FR 9013193 A FR9013193 A FR 9013193A FR 2659061 B1 FR2659061 B1 FR 2659061B1
Authority
FR
France
Prior art keywords
satellite
stabilizing
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
FR909013193A
Other languages
English (en)
Other versions
FR2659061A1 (fr
Inventor
Linder David Mark
Goodzeit Neil Evanscharzs Marc
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2659061A1 publication Critical patent/FR2659061A1/fr
Application granted granted Critical
Publication of FR2659061B1 publication Critical patent/FR2659061B1/fr
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
    • B64G1/28—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
    • B64G1/244—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
    • B64G1/283—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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR909013193A 1990-03-05 1990-10-24 Procede de stabilisation d'un satellite. Expired - Fee Related FR2659061B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/488,919 US5123617A (en) 1990-03-05 1990-03-05 Spacecraft momentum unloading using controlled magnetic torques

Publications (2)

Publication Number Publication Date
FR2659061A1 FR2659061A1 (fr) 1991-09-06
FR2659061B1 true FR2659061B1 (fr) 1992-05-22

Family

ID=23941669

Family Applications (1)

Application Number Title Priority Date Filing Date
FR909013193A Expired - Fee Related FR2659061B1 (fr) 1990-03-05 1990-10-24 Procede de stabilisation d'un satellite.

Country Status (2)

Country Link
US (1) US5123617A (fr)
FR (1) FR2659061B1 (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection
DE4432265C2 (de) * 1994-09-10 1996-12-12 Daimler Benz Aerospace Ag Verfahren zur Bestimmung des Drehimpulsvektors eines Satelliten
DE19518617A1 (de) * 1995-05-24 1996-11-28 Daimler Benz Aerospace Ag Dreiachsenstabilisierter, erdorientierter Satellit und zugehöriges Sonnen- und Erdakquisitonsverfahren unter Benutzung eines Magnetometers
FR2742243B1 (fr) * 1995-12-06 1998-02-13 Matra Marconi Space France Procede de commande d'attitude d'un satellite en orbite basse, a acquisition solaire
US6282467B1 (en) * 1997-10-14 2001-08-28 The Boeing Company Three-axis inertial attitude determination for spinning spacecraft
US6356814B1 (en) * 1999-02-03 2002-03-12 Microcosm, Inc. Spacecraft magnetic torquer feedback system
DE19924908B4 (de) * 1999-05-31 2008-05-29 Astrium Gmbh Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten
US6254036B1 (en) * 2000-02-16 2001-07-03 Hughes Electronics Corporation Method and apparatus for spacecraft wheel desaturation
US6292722B1 (en) * 2000-02-24 2001-09-18 Space Systems/Loral, Inc. Magnetic torquer control with thruster augmentation
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
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
US6600976B1 (en) * 2002-03-29 2003-07-29 Lockheed Martin Corporation Gyroless control system for zero-momentum three-axis stabilized spacecraft
US6702234B1 (en) 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
US20080099626A1 (en) * 2006-10-27 2008-05-01 Goodrich Corporation Reconfigurable reaction wheel for spacecraft
CN101819284B (zh) * 2010-05-18 2012-07-04 长安大学 一种利用陀螺仪测定地球极移的方法
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
CN105253326B (zh) * 2015-10-27 2017-12-05 上海微小卫星工程中心 一种微小卫星用开关磁矩时间序列控制方法
US10005568B2 (en) 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
CN106557090B (zh) * 2016-11-08 2019-06-28 上海宇航系统工程研究所 一种磁力线圈结合动量轮的航天器姿态联合控制方法
US11124320B2 (en) * 2019-02-12 2021-09-21 Canadian Space Agency Spacecraft control using residual dipole
CN110967144A (zh) * 2019-12-18 2020-04-07 中国科学院长春光学精密机械与物理研究所 一种磁力矩器标定装置
CN111056045B (zh) * 2019-12-26 2021-03-23 航天行云科技有限公司 一种三轴磁力矩器的控制方法以及装置
KR102250118B1 (ko) * 2020-03-25 2021-05-10 한국항공우주연구원 오프셋을 적용한 인공위성 반작용휠의 모멘텀 덤프 방법
GB2618066A (en) * 2022-04-19 2023-11-01 Iceye Polska Spolka Z Orgraniczona Odpowiedzialnoscia Determination of spacecraft inertial properties
CN115140318B (zh) * 2022-07-20 2023-05-05 南京理工大学 一种适用于微纳卫星大角速率消旋的磁阻尼控制方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3429524A (en) * 1965-07-19 1969-02-25 Westinghouse Electric Corp Attitude control system
JPS491439B1 (fr) * 1968-09-27 1974-01-14
US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
US3955858A (en) * 1974-01-03 1976-05-11 Societe Nationale Industrielle Aerospatiale Satellite momentum wheel
GB1544083A (en) * 1975-07-21 1979-04-11 Rca Corp Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits
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
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system

Also Published As

Publication number Publication date
FR2659061A1 (fr) 1991-09-06
US5123617A (en) 1992-06-23

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20070629