JP4249901B2 - 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御 - Google Patents

衛星の姿勢制御のための各運動量に基づくｃｍｇ制御 Download PDF

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Publication number
JP4249901B2
JP4249901B2 JP2000536623A JP2000536623A JP4249901B2 JP 4249901 B2 JP4249901 B2 JP 4249901B2 JP 2000536623 A JP2000536623 A JP 2000536623A JP 2000536623 A JP2000536623 A JP 2000536623A JP 4249901 B2 JP4249901 B2 JP 4249901B2
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value
angular momentum
signal
actuator position
control
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JP2000536623A
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Japanese (ja)
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JP2002506774A5 (enExample
JP2002506774A (ja
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ベイリー，デイビッド・エイ
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Honeywell International Inc
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Honeywell International Inc
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
    • B25J9/00—Programme-controlled manipulators
    • B25J9/16—Programme controls
    • B25J9/1602—Programme controls characterised by the control system, structure, architecture
    • B25J9/1607—Calculation of inertia, jacobian matrixes and inverses
    • 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)

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Automation & Control Theory (AREA)
  • Robotics (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP2000536623A 1998-03-16 1999-03-15 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御 Expired - Fee Related JP4249901B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/042,515 1998-03-16
US09/042,515 US6128556A (en) 1998-03-16 1998-03-16 CMG control based on angular momentum to control satellite attitude
PCT/US1999/005703 WO1999047420A1 (en) 1998-03-16 1999-03-15 Cmg control based on angular momentum to control satellite attitude

Publications (3)

Publication Number Publication Date
JP2002506774A JP2002506774A (ja) 2002-03-05
JP2002506774A5 JP2002506774A5 (enExample) 2006-04-27
JP4249901B2 true JP4249901B2 (ja) 2009-04-08

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ID=21922348

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Application Number Title Priority Date Filing Date
JP2000536623A Expired - Fee Related JP4249901B2 (ja) 1998-03-16 1999-03-15 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御

Country Status (5)

Country Link
US (1) US6128556A (enExample)
EP (1) EP1064197B1 (enExample)
JP (1) JP4249901B2 (enExample)
DE (1) DE69927005T2 (enExample)
WO (1) WO1999047420A1 (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6729580B2 (en) 2001-04-05 2004-05-04 Northrop Grumman Corporation Method and system for directing an object using gyroscopes
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
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
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
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
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
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
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
KR101517391B1 (ko) * 2013-12-27 2015-05-06 한국항공우주연구원 단일 입출력 제어기를 이용한 인공위성의 3축 자세 제어 시스템
US20250242908A1 (en) * 2024-01-29 2025-07-31 Textron Innovations Inc. Rotorcraft system for command mode transitions

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3606636C1 (de) * 1986-02-28 1987-11-05 Messerschmitt Boelkow Blohm Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
US5025381A (en) * 1990-01-02 1991-06-18 General Electric Company Attitude control compensator for flexible spacecraft
US5608634A (en) * 1992-06-12 1997-03-04 Martin Marietta Corp. Low noise spacecraft body rate sensing arrangement for attitude control
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
US5667171A (en) * 1995-04-28 1997-09-16 Hughes Aircraft Company Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device
US5765780A (en) * 1995-12-22 1998-06-16 Hughes Electronics Corporation Systematic vectored thrust calibration method for satellite momentum control
US5806804A (en) * 1996-11-12 1998-09-15 Lockheed Martin Corp. Adaptive harmonic disturbance compensation system

Also Published As

Publication number Publication date
DE69927005D1 (de) 2005-10-06
WO1999047420A1 (en) 1999-09-23
JP2002506774A (ja) 2002-03-05
US6128556A (en) 2000-10-03
EP1064197B1 (en) 2005-08-31
DE69927005T2 (de) 2006-06-14
EP1064197A1 (en) 2001-01-03

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