JP2008507446A5 - - Google Patents

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Publication number
JP2008507446A5
JP2008507446A5 JP2007522662A JP2007522662A JP2008507446A5 JP 2008507446 A5 JP2008507446 A5 JP 2008507446A5 JP 2007522662 A JP2007522662 A JP 2007522662A JP 2007522662 A JP2007522662 A JP 2007522662A JP 2008507446 A5 JP2008507446 A5 JP 2008507446A5
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JP
Japan
Prior art keywords
gimbal rate
space
command
cmg
calculating
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JP2007522662A
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English (en)
Japanese (ja)
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JP2008507446A (ja
JP4630332B2 (ja
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Priority claimed from US10/897,494 external-priority patent/US7246776B2/en
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Publication of JP2008507446A publication Critical patent/JP2008507446A/ja
Publication of JP2008507446A5 publication Critical patent/JP2008507446A5/ja
Application granted granted Critical
Publication of JP4630332B2 publication Critical patent/JP4630332B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2007522662A 2004-07-23 2005-07-18 Ｃｍｇアレイ特異性回避のための方法及びシステム Expired - Fee Related JP4630332B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/897,494 US7246776B2 (en) 2004-07-23 2004-07-23 Method and system for CMG array singularity avoidance
PCT/US2005/025614 WO2006085996A1 (en) 2004-07-23 2005-07-18 Method and system for cmg array singularity avoidance

Publications (3)

Publication Number Publication Date
JP2008507446A JP2008507446A (ja) 2008-03-13
JP2008507446A5 true JP2008507446A5 (enExample) 2008-05-15
JP4630332B2 JP4630332B2 (ja) 2011-02-09

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ID=35756501

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JP2007522662A Expired - Fee Related JP4630332B2 (ja) 2004-07-23 2005-07-18 Ｃｍｇアレイ特異性回避のための方法及びシステム

Country Status (5)

Country Link
US (1) US7246776B2 (enExample)
EP (1) EP1776626B1 (enExample)
JP (1) JP4630332B2 (enExample)
DE (1) DE602005012109D1 (enExample)
WO (1) WO2006085996A1 (enExample)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7246776B2 (en) 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance
US7370833B2 (en) * 2005-10-20 2008-05-13 Honeywell International Inc. Method and system for determining a singularity free momentum path
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
US7805226B2 (en) * 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
US7627404B2 (en) * 2007-04-13 2009-12-01 The Boeing Company Singularity escape and avoidance using a virtual array rotation
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
US8014911B2 (en) * 2009-11-03 2011-09-06 Honeywell International Inc. Methods and systems for imposing a momentum boundary while reorienting an agile vehicle with control moment gyroscopes
US8346538B2 (en) 2010-05-25 2013-01-01 Honeywell International Inc. Methods and systems for reducing angular velocity using a gyroscope array
US9567112B1 (en) 2013-06-27 2017-02-14 The United States Of America, As Represented By The Secretary Of The Navy Method and apparatus for singularity avoidance for control moment gyroscope (CMG) systems without using null motion
CN103940451B (zh) * 2014-04-30 2016-08-24 北京控制工程研究所 基于零空间向量自主优化选择的冗余陀螺故障定位方法
CN104044756B (zh) * 2014-06-09 2016-04-27 中国科学院长春光学精密机械与物理研究所 高集成高精度控制力矩陀螺群伺服控制装置
CN110712768B (zh) * 2019-10-31 2021-03-16 上海航天控制技术研究所 一种控制力矩陀螺群初始框架位置确定方法
CN112256048B (zh) * 2020-10-13 2022-02-11 北京航空航天大学 一种混合灵敏度优化的cmg框架系统速度调节方法
CN113247310B (zh) * 2021-05-20 2022-07-29 上海卫星工程研究所 一种适用于卫星可连续姿态机动次数的估算方法及系统
US20240308698A1 (en) * 2023-03-08 2024-09-19 The Boeing Company Systems and methods for combined control moment gyroscope and thruster control
CN119160416B (zh) * 2024-11-20 2025-02-25 杭州电子科技大学 一种基于前馈模型预测的立体成像卫星姿态控制方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2678894B1 (fr) * 1991-07-09 1993-11-19 Aerospatiale Ste Nationale Indle Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.
US5875676A (en) * 1997-09-02 1999-03-02 Honeywell Inc. Non colocated rate sensing for control moment gyroscopes
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
US6128556A (en) * 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
US6047927A (en) * 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control
US6039290A (en) 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
US6360996B1 (en) * 2000-02-24 2002-03-26 Hughes Electronics Corporation Steering control for skewed scissors pair CMG clusters
US6354163B1 (en) 2000-05-17 2002-03-12 Honeywell International Inc. Mitigating gimbal induced disturbances in CMG arrays
JP2002145199A (ja) * 2000-11-13 2002-05-22 Toshiba Corp 宇宙航行体の姿勢制御装置
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
US6681649B2 (en) * 2002-04-03 2004-01-27 Honeywell International Inc. Inertial control and measurement system
US6648274B1 (en) * 2002-04-12 2003-11-18 David A. Bailey Virtual reaction wheel array
AU2003294218A1 (en) * 2002-08-28 2004-04-23 Arizona Board Of Regents Steering logic for control moment gyro system
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
US7246776B2 (en) 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance

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