CA2452250C - Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes - Google Patents

Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes Download PDF

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Publication number
CA2452250C
CA2452250C CA2452250A CA2452250A CA2452250C CA 2452250 C CA2452250 C CA 2452250C CA 2452250 A CA2452250 A CA 2452250A CA 2452250 A CA2452250 A CA 2452250A CA 2452250 C CA2452250 C CA 2452250C
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CA
Canada
Prior art keywords
configuration
actuators
cluster
satellite
attitude
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
CA2452250A
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English (en)
French (fr)
Other versions
CA2452250A1 (fr
Inventor
Kristen Lagadec
Ange Defendini
Julien Morand
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
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EADS Astrium SAS
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Filing date
Publication date
Application filed by EADS Astrium SAS filed Critical EADS Astrium SAS
Publication of CA2452250A1 publication Critical patent/CA2452250A1/fr
Application granted granted Critical
Publication of CA2452250C publication Critical patent/CA2452250C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • B64G1/244—Spacecraft control systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radio Relay Systems (AREA)
CA2452250A 2001-06-26 2002-06-24 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes Expired - Lifetime CA2452250C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0108409A FR2826470B1 (fr) 2001-06-26 2001-06-26 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes
FR01/08409 2001-06-26
PCT/FR2002/002181 WO2003001311A1 (fr) 2001-06-26 2002-06-24 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes

Publications (2)

Publication Number Publication Date
CA2452250A1 CA2452250A1 (fr) 2003-01-03
CA2452250C true CA2452250C (fr) 2014-12-23

Family

ID=8864776

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2452250A Expired - Lifetime CA2452250C (fr) 2001-06-26 2002-06-24 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes

Country Status (10)

Country Link
US (1) US7171290B2 (enExample)
EP (1) EP1407335B1 (enExample)
JP (1) JP4307247B2 (enExample)
AT (1) ATE341783T1 (enExample)
CA (1) CA2452250C (enExample)
DE (1) DE60215174T2 (enExample)
ES (1) ES2274088T3 (enExample)
FR (1) FR2826470B1 (enExample)
IL (2) IL159573A0 (enExample)
WO (1) WO2003001311A1 (enExample)

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JP5556782B2 (ja) * 2011-10-04 2014-07-23 三菱電機株式会社 人工衛星の姿勢制御装置
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
CN102566578B (zh) * 2012-01-12 2013-06-19 北京航空航天大学 基于奇异值分解的单框架控制力矩陀螺群协调控制方法
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CN104460427B (zh) * 2014-10-31 2017-01-25 上海卫星工程研究所 模块化微型卫星平台综合电子系统
CN104527994B (zh) * 2015-01-21 2016-08-24 哈尔滨工业大学 异面交叉快变轨道固定时间稳定姿态指向跟踪控制方法
KR101654282B1 (ko) * 2015-02-13 2016-09-05 홍대안 다중 모멘텀 휠 어셈블리를 적용한 제어 모멘트 자이로
US10407187B2 (en) 2015-06-22 2019-09-10 Mitsubishi Electric Corporation Device for controlling attitude of spacecraft and method for calculating CMG gimbal angle
FR3038082B1 (fr) * 2015-06-24 2017-07-07 Centre Nat D'etudes Spatiales (Cnes) Procede d'evitement d'une zone interdite par un satellite
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CN106020224B (zh) * 2016-07-22 2019-01-08 北京航空航天大学 一种考虑质心位置不确定性的上面级矢量推力控制方法
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US6682019B2 (en) * 2002-04-04 2004-01-27 Honeywell International Inc. Minimum energy wheel configurations for energy storage and attitude control

Also Published As

Publication number Publication date
WO2003001311A1 (fr) 2003-01-03
ES2274088T3 (es) 2007-05-16
US7171290B2 (en) 2007-01-30
JP4307247B2 (ja) 2009-08-05
EP1407335B1 (fr) 2006-10-04
IL159573A0 (en) 2004-06-01
EP1407335A1 (fr) 2004-04-14
DE60215174D1 (de) 2006-11-16
DE60215174T2 (de) 2007-08-23
FR2826470A1 (fr) 2002-12-27
US20040167683A1 (en) 2004-08-26
FR2826470B1 (fr) 2003-09-19
IL159573A (en) 2008-11-03
JP2004535324A (ja) 2004-11-25
CA2452250A1 (fr) 2003-01-03
ATE341783T1 (de) 2006-10-15

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