DE69927005T2 - Steuerung von momentumsregelungsgyroskopen nach dem drehimpuls zur lageregelung eines satellits - Google Patents

Steuerung von momentumsregelungsgyroskopen nach dem drehimpuls zur lageregelung eines satellits Download PDF

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Publication number
DE69927005T2
DE69927005T2 DE69927005T DE69927005T DE69927005T2 DE 69927005 T2 DE69927005 T2 DE 69927005T2 DE 69927005 T DE69927005 T DE 69927005T DE 69927005 T DE69927005 T DE 69927005T DE 69927005 T2 DE69927005 T2 DE 69927005T2
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DE
Germany
Prior art keywords
control
satellite
locating
rotating pulse
moment
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
DE69927005T
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German (de)
English (en)
Other versions
DE69927005D1 (de
Inventor
A Bailey
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
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Publication date
Application filed by Honeywell Inc filed Critical Honeywell Inc
Publication of DE69927005D1 publication Critical patent/DE69927005D1/de
Application granted granted Critical
Publication of DE69927005T2 publication Critical patent/DE69927005T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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)

Landscapes

  • 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)
DE69927005T 1998-03-16 1999-03-15 Steuerung von momentumsregelungsgyroskopen nach dem drehimpuls zur lageregelung eines satellits Expired - Lifetime DE69927005T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (2)

Publication Number Publication Date
DE69927005D1 DE69927005D1 (de) 2005-10-06
DE69927005T2 true DE69927005T2 (de) 2006-06-14

Family

ID=21922348

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69927005T Expired - Lifetime DE69927005T2 (de) 1998-03-16 1999-03-15 Steuerung von momentumsregelungsgyroskopen nach dem drehimpuls zur lageregelung eines satellits

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
JP4249901B2 (ja) 2009-04-08
EP1064197A1 (en) 2001-01-03

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