JP2004538439A5 - - Google Patents

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Publication number
JP2004538439A5
JP2004538439A5 JP2001508660A JP2001508660A JP2004538439A5 JP 2004538439 A5 JP2004538439 A5 JP 2004538439A5 JP 2001508660 A JP2001508660 A JP 2001508660A JP 2001508660 A JP2001508660 A JP 2001508660A JP 2004538439 A5 JP2004538439 A5 JP 2004538439A5
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JP
Japan
Prior art keywords
control moment
wedge
momentum
pair
vehicle
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.)
Granted
Application number
JP2001508660A
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English (en)
Japanese (ja)
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JP2004538439A (ja
JP4354144B2 (ja
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Publication date
Priority claimed from US09/340,806 external-priority patent/US6241194B1/en
Application filed filed Critical
Publication of JP2004538439A publication Critical patent/JP2004538439A/ja
Publication of JP2004538439A5 publication Critical patent/JP2004538439A5/ja
Application granted granted Critical
Publication of JP4354144B2 publication Critical patent/JP4354144B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001508660A 1999-06-28 2000-06-28 輸送手段用制御システム Expired - Fee Related JP4354144B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/340,806 US6241194B1 (en) 1999-06-28 1999-06-28 Momentum position control
PCT/US2000/017717 WO2001002921A2 (en) 1999-06-28 2000-06-28 Momentum position control

Publications (3)

Publication Number Publication Date
JP2004538439A JP2004538439A (ja) 2004-12-24
JP2004538439A5 true JP2004538439A5 (enExample) 2007-05-10
JP4354144B2 JP4354144B2 (ja) 2009-10-28

Family

ID=23335015

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001508660A Expired - Fee Related JP4354144B2 (ja) 1999-06-28 2000-06-28 輸送手段用制御システム

Country Status (8)

Country Link
US (1) US6241194B1 (enExample)
EP (1) EP1188098B1 (enExample)
JP (1) JP4354144B2 (enExample)
AT (1) ATE259078T1 (enExample)
AU (1) AU1324001A (enExample)
CA (1) CA2378157A1 (enExample)
DE (1) DE60008103T2 (enExample)
WO (1) WO2001002921A2 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2796172B1 (fr) * 1999-07-08 2001-09-21 Cit Alcatel Systeme pour le controle d'un satellite en attitude et procede corespondant
US6354163B1 (en) * 2000-05-17 2002-03-12 Honeywell International Inc. Mitigating gimbal induced disturbances in CMG arrays
US6515221B1 (en) * 2000-08-01 2003-02-04 Honeywell International Inc. Modular reaction wheel assembly to shield electronics on a satellite
FR2846107B1 (fr) * 2002-10-21 2005-06-24 Cit Alcatel Dispositif de controle d'attitude d'un satellite geostationnaire
FR2861690B1 (fr) * 2003-11-04 2006-04-07 Eads Astrium Sas Controle d'attitude de satellites en particulier agiles a nombre reduit de gyrodynes
US7014150B2 (en) * 2004-07-30 2006-03-21 Honeywell International Inc. Method and system for optimizing torque in a CMG array
US7627404B2 (en) * 2007-04-13 2009-12-01 The Boeing Company Singularity escape and avoidance using a virtual array rotation
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
US8561944B2 (en) 2010-06-17 2013-10-22 Lockheed Martin Corporation System and method for desaturation of a control moment gyroscope
US20120160965A1 (en) * 2010-12-23 2012-06-28 Muller Ronald M Method to achieve a rapid and low power slew of a satellite
EP3304234A4 (en) * 2015-06-02 2019-01-16 The Charles Stark Draper Laboratory, Inc. SYSTEMS FOR QUICK PANS AND CALM FOR SMALL SATELLITES
US9551994B2 (en) 2015-06-15 2017-01-24 The Boeing Company System and method for vehicle attitude control
EP3559702B1 (en) * 2016-12-22 2024-04-24 Myriota Pty Ltd System and method for generating extended satellite ephemeris data

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
DE4129628A1 (de) * 1991-09-06 1993-03-18 Deutsche Aerospace Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges
US5681012A (en) * 1995-01-05 1997-10-28 Hughes Electronics Spacecraft control with skewed control moment gyros
DE19510371C1 (de) * 1995-03-22 1996-10-31 Daimler Benz Aerospace Ag Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit
JP2937123B2 (ja) * 1995-06-15 1999-08-23 日本電気株式会社 宇宙航行体及び宇宙航行体の姿勢制御方法
JPH09226696A (ja) * 1996-02-22 1997-09-02 Toshiba Corp 人工衛星姿勢制御装置
US6053445A (en) * 1996-09-09 2000-04-25 C-1 Design Group Fly fishing reel with isolated conical drag
US6062512A (en) * 1997-08-27 2000-05-16 Hughes Electronics Corporation Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices
US6047927A (en) * 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control

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