DE69942590D1 - Gyroskopischer Stellantrieb, insbesondere für die Lageregelung eines Satelliten - Google Patents

Gyroskopischer Stellantrieb, insbesondere für die Lageregelung eines Satelliten

Info

Publication number
DE69942590D1
DE69942590D1 DE69942590T DE69942590T DE69942590D1 DE 69942590 D1 DE69942590 D1 DE 69942590D1 DE 69942590 T DE69942590 T DE 69942590T DE 69942590 T DE69942590 T DE 69942590T DE 69942590 D1 DE69942590 D1 DE 69942590D1
Authority
DE
Germany
Prior art keywords
satellite
position control
gyroscopic actuator
gyroscopic
actuator
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
DE69942590T
Other languages
English (en)
Inventor
Ange Defendini
Kristen Lagadec
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 Defence and Space SAS
Original Assignee
EADS Astrium 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 EADS Astrium SAS filed Critical EADS Astrium SAS
Application granted granted Critical
Publication of DE69942590D1 publication Critical patent/DE69942590D1/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
    • B64G1/28—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
    • B64G1/244—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
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • 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
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
    • G01C19/06—Rotors
    • G01C19/08—Rotors electrically driven

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Gyroscopes (AREA)
  • Toys (AREA)
DE69942590T 1998-11-19 1999-07-21 Gyroskopischer Stellantrieb, insbesondere für die Lageregelung eines Satelliten Expired - Lifetime DE69942590D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9814548A FR2786283B1 (fr) 1998-11-19 1998-11-19 Procede et dispositif de pilotage de l'attitude d'un satellite

Publications (1)

Publication Number Publication Date
DE69942590D1 true DE69942590D1 (de) 2010-08-26

Family

ID=9532924

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69942590T Expired - Lifetime DE69942590D1 (de) 1998-11-19 1999-07-21 Gyroskopischer Stellantrieb, insbesondere für die Lageregelung eines Satelliten
DE69926854T Expired - Lifetime DE69926854T2 (de) 1998-11-19 1999-07-21 Methode und Vorrichtung zur Lageregelung eines Satelliten

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE69926854T Expired - Lifetime DE69926854T2 (de) 1998-11-19 1999-07-21 Methode und Vorrichtung zur Lageregelung eines Satelliten

Country Status (5)

Country Link
US (1) US6305647B1 (de)
EP (2) EP1484247B1 (de)
DE (2) DE69942590D1 (de)
ES (2) ES2345487T3 (de)
FR (1) FR2786283B1 (de)

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* Cited by examiner, † Cited by third party
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FR2786283B1 (fr) 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
US6454218B1 (en) * 2000-02-28 2002-09-24 Quoin International, Inc. Integrated system for providing 3-axis attitude-control, energy-storage, and electrical power
FR2819597B1 (fr) 2001-01-15 2003-04-11 Cit Alcatel Procede de guidage d'un systeme d'actionneurs gyrospcopiques
US6729580B2 (en) * 2001-04-05 2004-05-04 Northrop Grumman Corporation Method and system for directing an object using gyroscopes
FR2826470B1 (fr) * 2001-06-26 2003-09-19 Astrium Sas Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes
US6691955B2 (en) * 2001-11-27 2004-02-17 Space Systems/Loral Spacecraft having a momentum wheel configuration that prevents zero wheel speeds
FR2837580B1 (fr) 2002-03-21 2005-06-03 Astrium Sas Actionneur gyroscopique de pilotage de l'attitude d'un vehicule spatial
US6682019B2 (en) * 2002-04-04 2004-01-27 Honeywell International Inc. Minimum energy wheel configurations for energy storage and attitude control
JP3970724B2 (ja) * 2002-08-30 2007-09-05 Ｎｅｃ東芝スペースシステム株式会社 飛翔体の姿勢変更制御装置及び姿勢変更制御方法
US7152495B2 (en) * 2002-12-19 2006-12-26 Honeywell International, Inc. System and method for adaptive cancellation of disturbances
US6758444B1 (en) * 2002-12-30 2004-07-06 Honeywell International Inc. Momentum control system and method
FR2850948B1 (fr) 2003-02-07 2006-01-06 Astrium Sas Dispositif de pilotage de l'attitude d'un satellite par actionneurs gyroscopiques
US6779759B1 (en) * 2003-03-28 2004-08-24 Honeywell International, Inc. Integrated power and attitude control system and method
FR2858294A1 (fr) * 2003-07-28 2005-02-04 Eads Astrium Sas Roue d'inertie pour vehicule
US7561947B2 (en) * 2003-10-06 2009-07-14 Honeywell International Inc. Dynamic CMG array and method
FR2861690B1 (fr) 2003-11-04 2006-04-07 Eads Astrium Sas Controle d'attitude de satellites en particulier agiles a nombre reduit de gyrodynes
US7185855B2 (en) * 2004-04-30 2007-03-06 Honeywell International, Inc. Method and system for steering a momentum control system
US7364120B2 (en) * 2004-08-26 2008-04-29 Honeywell International, Inc. Quantized control-moment gyroscope array
KR100552583B1 (ko) 2004-11-16 2006-02-15 한국과학기술원 특이점 문제를 개선한 제어 모멘트 자이로스코프 및 그구동 방법
US7693619B2 (en) 2005-11-30 2010-04-06 Honeywell International Inc. Method and system for controlling sets of collinear control moment gyroscopes with offset determination without attitude trajectory of spacecraft
GB0606885D0 (en) * 2006-04-05 2006-05-17 Suisse Electronique Microtech Torquer apparatus
KR100778098B1 (ko) 2006-07-26 2007-11-22 한국항공우주연구원 인공위성 3축 자세제어용 제어 모멘트 자이로 클러스터
US7805226B2 (en) * 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
FR2907423B1 (fr) * 2006-10-23 2009-07-03 Astrium Sas Soc Par Actions Si Gyrodyne et son dispositif de montage
GB2445569A (en) * 2007-01-12 2008-07-16 Duncan James Harrison Gyro-coupling torque converter
US20090039202A1 (en) * 2007-02-07 2009-02-12 Keita Ogo Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium
JP4463287B2 (ja) * 2007-02-07 2010-05-19 Ｎｅｃ東芝スペースシステム株式会社 姿勢変更制御方法、姿勢変更制御システム、姿勢変更制御プログラムおよびプログラム記録媒体
US7997157B2 (en) * 2008-02-11 2011-08-16 Honeywell International Inc. Control moment gyroscope
US8127631B2 (en) * 2008-09-17 2012-03-06 Honeywell International Inc. Rotor assembly including strain relief feature
US8688296B2 (en) * 2008-11-17 2014-04-01 David A. Bailey Method for maximum data collection with a control moment gyroscope controlled satellite
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
WO2010135421A2 (en) 2009-05-19 2010-11-25 University Of Florida Research Foundation, Inc. Attitude control system for small satellites
US8312782B2 (en) * 2009-06-18 2012-11-20 Honeywell International Inc. Control moment gyroscope based momentum control systems in small satellites
FR2981050B1 (fr) * 2011-10-07 2014-07-25 Larminat Philippe De Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile
US9061775B2 (en) * 2012-06-22 2015-06-23 Isaac M. Ross Method and apparatus for spacecraft attitude control using polynomial interpolation
US8880246B1 (en) * 2012-08-22 2014-11-04 United States Of America As Represented By The Secretary Of The Navy Method and apparatus for determining spacecraft maneuvers
US9849785B1 (en) * 2012-12-10 2017-12-26 The United States Of America, As Represented By The Secretary Of The Navy Method and apparatus for state space trajectory control of uncertain dynamical systems
CN104699107B (zh) * 2015-02-05 2017-10-13 北京理工大学 一种控制力矩陀螺群的桁架包络结构的搭建方法
US10114382B2 (en) * 2016-05-10 2018-10-30 Sikorsky Aircraft Corporation Flexible command model for aircraft control
JP6556371B2 (ja) * 2016-09-09 2019-08-07 三菱電機株式会社 姿勢制御装置、姿勢制御システム、地上局、人工衛星、姿勢制御方法及びプログラム
CN106553771A (zh) * 2016-10-21 2017-04-05 上海卫星工程研究所 适用于五棱锥构形布局的sgcmg一体化支撑装置
FR3074685B1 (fr) 2017-12-12 2019-11-22 Societe D'exploitation De Produits Pour Les Industries Chimiques Seppic Nouveaux polyol polyrhamnosides, procede pour leur preparation et composition cosmetiques et/ou pharmaceutiques en comprenant
FR3074686B1 (fr) 2017-12-12 2019-11-15 Societe D'exploitation De Produits Pour Les Industries Chimiques Seppic Nouveaux glyceryl polyrhamnosides, procede pour leur preparation et composition cosmetiques et/ou pharmaceutiques en comprenant
CN108146659A (zh) * 2018-02-08 2018-06-12 黄君 卫星姿态控制磁力矩、卫星姿态控制系统及卫星
CN111099040B (zh) * 2019-10-18 2021-10-29 上海航天控制技术研究所 一种基于控制力矩陀螺群控制的系统极性确定方法
CN113917958B (zh) * 2021-08-31 2023-05-09 北京控制工程研究所 一种三浮陀螺单机在轨自主管理与控制方法

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US3452948A (en) * 1967-01-03 1969-07-01 Garrett Corp System and method for free body stabilization and orientation
US3603161A (en) * 1969-09-04 1971-09-07 Bodenseewerk Geraetetech Gyroscope with collectorless dc motor
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
FR2384174A1 (fr) * 1977-03-15 1978-10-13 Aerospatiale Roue d'inertie
US4375878A (en) * 1980-10-28 1983-03-08 Lockheed Missiles & Space Company, Inc. Space satellite with agile payload orientation system
US4573651A (en) * 1983-12-19 1986-03-04 Stanton Austin N Torque orientation device
JPH01226496A (ja) 1988-03-07 1989-09-11 Toshiba Corp 宇宙航行体の姿勢制御装置
US5256942A (en) * 1992-05-07 1993-10-26 Wood Ross C Stabilization system for a freely rotatable platform
WO1994010036A1 (de) * 1992-10-27 1994-05-11 Teldix Gmbh Einrichtung zum schwenken eines flugkörpers, mit zwei kreiseln
US5386738A (en) * 1992-12-22 1995-02-07 Honeywell Inc. Direct torque control moment gyroscope
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft
US5681012A (en) * 1995-01-05 1997-10-28 Hughes Electronics Spacecraft control with skewed control moment gyros
US5692707A (en) * 1995-05-15 1997-12-02 Hughes Aircraft Company Universal spacecraft attitude steering control system
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
US6039290A (en) * 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
FR2786283B1 (fr) 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite

Also Published As

Publication number Publication date
EP1484247B1 (de) 2010-07-14
ES2345487T3 (es) 2010-09-24
FR2786283A1 (fr) 2000-05-26
FR2786283B1 (fr) 2001-01-26
EP1002716A1 (de) 2000-05-24
US6305647B1 (en) 2001-10-23
EP1484247A1 (de) 2004-12-08
EP1002716B1 (de) 2005-08-24
DE69926854D1 (de) 2005-09-29
ES2247767T3 (es) 2006-03-01
DE69926854T2 (de) 2006-06-29

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