DE602005012109D1 - Verfahren und system zur cmg-anordnung-singularitätsvermeidung - Google Patents

Verfahren und system zur cmg-anordnung-singularitätsvermeidung

Info

Publication number
DE602005012109D1
DE602005012109D1 DE602005012109T DE602005012109T DE602005012109D1 DE 602005012109 D1 DE602005012109 D1 DE 602005012109D1 DE 602005012109 T DE602005012109 T DE 602005012109T DE 602005012109 T DE602005012109 T DE 602005012109T DE 602005012109 D1 DE602005012109 D1 DE 602005012109D1
Authority
DE
Germany
Prior art keywords
singularity avoidance
cmg
arrangement
cmg arrangement
singularity
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
DE602005012109T
Other languages
German (de)
English (en)
Inventor
Mason A Peck
Brian Underhill
Brian J Hamilton
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.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of DE602005012109D1 publication Critical patent/DE602005012109D1/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
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE602005012109T 2004-07-23 2005-07-18 Verfahren und system zur cmg-anordnung-singularitätsvermeidung Expired - Lifetime DE602005012109D1 (de)

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 (1)

Publication Number Publication Date
DE602005012109D1 true DE602005012109D1 (de) 2009-02-12

Family

ID=35756501

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005012109T Expired - Lifetime DE602005012109D1 (de) 2004-07-23 2005-07-18 Verfahren und system zur cmg-anordnung-singularitätsvermeidung

Country Status (5)

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

Families Citing this family (15)

* 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
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.
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
US5875676A (en) * 1997-09-02 1999-03-02 Honeywell Inc. Non colocated rate sensing for control moment gyroscopes
US6039290A (en) 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
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
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
US6917862B2 (en) * 2002-08-28 2005-07-12 Arizona Board Of Regents Singularity escape/avoidance steering logic for control moment gyro systems
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

Also Published As

Publication number Publication date
EP1776626A1 (en) 2007-04-25
US20060027708A1 (en) 2006-02-09
EP1776626B1 (en) 2008-12-31
US7246776B2 (en) 2007-07-24
JP2008507446A (ja) 2008-03-13
JP4630332B2 (ja) 2011-02-09
WO2006085996A1 (en) 2006-08-17

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