DE69911184D1 - Ständige raumfahrzeugslageregelung, wobei singularitätszustände bei der kontrollmomentumsgyroanordnung vermieden werden - Google Patents

Ständige raumfahrzeugslageregelung, wobei singularitätszustände bei der kontrollmomentumsgyroanordnung vermieden werden

Info

Publication number
DE69911184D1
DE69911184D1 DE69911184T DE69911184T DE69911184D1 DE 69911184 D1 DE69911184 D1 DE 69911184D1 DE 69911184 T DE69911184 T DE 69911184T DE 69911184 T DE69911184 T DE 69911184T DE 69911184 D1 DE69911184 D1 DE 69911184D1
Authority
DE
Germany
Prior art keywords
singularity
avoided
states
control torque
vehicle storage
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
DE69911184T
Other languages
English (en)
Other versions
DE69911184T2 (de
Inventor
A Bailey
J Heiberg
Bong Wie
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 Inc
Original Assignee
Honeywell 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 Inc filed Critical Honeywell Inc
Application granted granted Critical
Publication of DE69911184D1 publication Critical patent/DE69911184D1/de
Publication of DE69911184T2 publication Critical patent/DE69911184T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D23/00—Control of temperature
    • G05D23/19—Control of temperature characterised by the use of electric means
    • G05D23/1902—Control of temperature characterised by the use of electric means characterised by the use of a variable reference value
    • G05D23/1904—Control of temperature characterised by the use of electric means characterised by the use of a variable reference value variable in time
    • 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)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (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)
DE69911184T 1998-03-16 1999-03-15 Ständige raumfahrzeugslageregelung, wobei singularitätszustände bei der kontrollmomentumsgyroanordnung vermieden werden Expired - Lifetime DE69911184T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US39869 1998-03-16
US09/039,869 US6131056A (en) 1998-03-16 1998-03-16 Continuous attitude control that avoids CMG array singularities
PCT/US1999/005596 WO1999052021A2 (en) 1998-03-16 1999-03-15 Continuous spacecraft attitude control that avoids cmg array singularities

Publications (2)

Publication Number Publication Date
DE69911184D1 true DE69911184D1 (de) 2003-10-16
DE69911184T2 DE69911184T2 (de) 2004-06-03

Family

ID=21907762

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69911184T Expired - Lifetime DE69911184T2 (de) 1998-03-16 1999-03-15 Ständige raumfahrzeugslageregelung, wobei singularitätszustände bei der kontrollmomentumsgyroanordnung vermieden werden

Country Status (6)

Country Link
US (1) US6131056A (de)
EP (1) EP1064591B1 (de)
JP (1) JP2002510816A (de)
DE (1) DE69911184T2 (de)
RU (1) RU2000125884A (de)
WO (1) WO1999052021A2 (de)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
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AU5021999A (en) * 1998-07-23 2000-02-14 Bristol Aerospace Limited System and method for spacecraft 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
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
US6891498B2 (en) 2002-03-28 2005-05-10 Honeywell International Inc. Inertial reference system for a spacecraft
US6682019B2 (en) * 2002-04-04 2004-01-27 Honeywell International Inc. Minimum energy wheel configurations for energy storage and attitude control
EP1514257A4 (de) 2002-04-12 2015-12-30 Henry K Obermeyer Mehrachsen-joystick und wandlermittel dafür
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
US7561947B2 (en) * 2003-10-06 2009-07-14 Honeywell International Inc. Dynamic CMG array and method
US7246776B2 (en) * 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance
US7014150B2 (en) * 2004-07-30 2006-03-21 Honeywell International Inc. Method and system for optimizing torque in a CMG array
US7364120B2 (en) * 2004-08-26 2008-04-29 Honeywell International, Inc. Quantized control-moment gyroscope array
JP4511390B2 (ja) * 2005-03-01 2010-07-28 三菱電機株式会社 人工衛星の姿勢制御装置
US7464899B2 (en) * 2005-08-03 2008-12-16 Honeywell International Inc. Method and system for determining a singularity free momentum path
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
JP4679439B2 (ja) * 2006-06-05 2011-04-27 三菱電機株式会社 人工衛星の姿勢制御装置
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
US7627404B2 (en) * 2007-04-13 2009-12-01 The Boeing Company Singularity escape and avoidance using a virtual array rotation
JP5228641B2 (ja) * 2008-06-16 2013-07-03 三菱電機株式会社 姿勢制御装置および位置制御装置
FR2937954B1 (fr) * 2008-10-31 2011-07-29 Thales Sa Procede et systeme de desaturation des roues d'inertie d'un engin spatial
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
JP5126107B2 (ja) * 2009-02-19 2013-01-23 三菱電機株式会社 人工衛星の姿勢制御装置
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
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
US9038958B1 (en) * 2012-05-29 2015-05-26 United States Of America As Represented By The Secretary Of The Navy Method and apparatus for contingency guidance of a CMG-actuated spacecraft
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
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
CN103455035B (zh) * 2013-08-26 2015-12-23 北京理工大学 基于反步设计和非线性反馈的pd+姿态控制律设计方法
KR101517391B1 (ko) * 2013-12-27 2015-05-06 한국항공우주연구원 단일 입출력 제어기를 이용한 인공위성의 3축 자세 제어 시스템
CN104102224B (zh) * 2014-06-24 2016-09-07 上海微小卫星工程中心 一种双回路卫星姿态跟踪控制装置及方法
CN105905187A (zh) * 2016-06-22 2016-08-31 北京科技大学 仿生正六边形六足机器人

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US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
US3813067A (en) * 1972-06-29 1974-05-28 Trw Inc Attitude stabilization system
US3968352A (en) * 1974-05-17 1976-07-06 Sperry Rand Corporation Torque control system for reaction wheel assemblies and the like
GB1544083A (en) * 1975-07-21 1979-04-11 Rca Corp Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
DE3071249D1 (en) * 1980-08-19 1986-01-02 Messerschmitt Boelkow Blohm Attitude control device for elastic vehicles
US4489383A (en) * 1981-10-16 1984-12-18 Rca Corporation Closed-loop magnetic roll/yaw control system for high inclination orbit satellites
US4893254A (en) * 1988-04-20 1990-01-09 University Of British Columbia Manipulator arm position sensing
US5080307A (en) * 1990-05-14 1992-01-14 Hughes Aircraft Company Spacecraft earth-pointing attitude acquisition method
US5276390A (en) * 1991-10-04 1994-01-04 Hewlett-Packard Company System for hybrid position and force control
US5499320A (en) * 1993-03-24 1996-03-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Extended task space control for robotic manipulators
SE9400579L (sv) * 1994-02-21 1995-08-22 Asea Brown Boveri Förfarande för att styra en industrirobots rörelse i och i närheten av singulariteter
GB9403644D0 (en) * 1994-02-25 1994-04-13 Advanced Robotics Res Manipulator controller
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

Also Published As

Publication number Publication date
DE69911184T2 (de) 2004-06-03
WO1999052021A2 (en) 1999-10-14
JP2002510816A (ja) 2002-04-09
EP1064591A2 (de) 2001-01-03
US6131056A (en) 2000-10-10
WO1999052021A3 (en) 1999-12-02
RU2000125884A (ru) 2002-09-10
EP1064591B1 (de) 2003-09-10

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