DE69925719T2 - Singularitätsvermeidung in einer cmg satellitenlageregelung - Google Patents

Singularitätsvermeidung in einer cmg satellitenlageregelung Download PDF

Info

Publication number
DE69925719T2
DE69925719T2 DE69925719T DE69925719T DE69925719T2 DE 69925719 T2 DE69925719 T2 DE 69925719T2 DE 69925719 T DE69925719 T DE 69925719T DE 69925719 T DE69925719 T DE 69925719T DE 69925719 T2 DE69925719 T2 DE 69925719T2
Authority
DE
Germany
Prior art keywords
signal
torque
control
singularity
cmg
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
DE69925719T
Other languages
German (de)
English (en)
Other versions
DE69925719D1 (de
Inventor
J. Christopher HEIBERG
A. David 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
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
Publication of DE69925719D1 publication Critical patent/DE69925719D1/de
Application granted granted Critical
Publication of DE69925719T2 publication Critical patent/DE69925719T2/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
    • 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
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors

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)
DE69925719T 1998-03-16 1999-03-16 Singularitätsvermeidung in einer cmg satellitenlageregelung Expired - Lifetime DE69925719T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/039,640 US6047927A (en) 1998-03-16 1998-03-16 Escaping singularities in a satellite attitude control
US39640 1998-03-16
PCT/US1999/005598 WO1999050144A2 (en) 1998-03-16 1999-03-16 Singularity avoidance in a cmg satellite attitude control

Publications (2)

Publication Number Publication Date
DE69925719D1 DE69925719D1 (de) 2005-07-14
DE69925719T2 true DE69925719T2 (de) 2006-03-23

Family

ID=21906571

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69925719T Expired - Lifetime DE69925719T2 (de) 1998-03-16 1999-03-16 Singularitätsvermeidung in einer cmg satellitenlageregelung

Country Status (5)

Country Link
US (1) US6047927A (enExample)
EP (1) EP1064196B1 (enExample)
JP (1) JP4249902B2 (enExample)
DE (1) DE69925719T2 (enExample)
WO (1) WO1999050144A2 (enExample)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6241194B1 (en) * 1999-06-28 2001-06-05 Honeywell International Inc. Momentum position control
US6191728B1 (en) * 1999-07-07 2001-02-20 Honeywell International Inc. Agile satellite targeting
US6711476B2 (en) 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US6591169B2 (en) 2001-09-27 2003-07-08 The Boeing Company Method and computer program product for controlling the actuators of an aerodynamic vehicle
US6732977B1 (en) 2002-02-11 2004-05-11 Lockheed Martin Corporation System for on-orbit correction of spacecraft payload pointing errors
US6695263B1 (en) 2002-02-12 2004-02-24 Lockheed Martin Corporation System for geosynchronous spacecraft rapid earth reacquisition
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6891498B2 (en) 2002-03-28 2005-05-10 Honeywell International Inc. Inertial reference system for a spacecraft
US6702234B1 (en) * 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum 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
US6917862B2 (en) * 2002-08-28 2005-07-12 Arizona Board Of Regents Singularity escape/avoidance steering logic for control moment gyro systems
US6814330B2 (en) * 2002-12-12 2004-11-09 The Boeing Company Method and computer program product for controlling the control effectors of an aerodynamic vehicle
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
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
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering 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
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
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
JP5484262B2 (ja) * 2010-08-31 2014-05-07 三菱電機株式会社 宇宙機の姿勢制御装置
US9849785B1 (en) * 2012-12-10 2017-12-26 The United States Of America, As Represented By The Secretary Of The Navy Method and apparatus for state space trajectory control of uncertain dynamical systems
IL223899A (en) 2012-12-26 2017-06-29 Israel Aerospace Ind Ltd Device control system, method and method
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
RU2562466C1 (ru) * 2014-04-29 2015-09-10 Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") Способ управления ориентацией космического аппарата и устройство, его реализующее
CN104238563B (zh) * 2014-09-04 2017-01-18 北京航空航天大学 可变面倾角的控制力矩陀螺群设计方法
CN104850128B (zh) * 2015-05-21 2017-09-19 上海新跃仪表厂 一种用于具有大惯量积航天器的动量轮布局配置方法
CN110576983B (zh) * 2019-08-26 2021-03-16 上海航天控制技术研究所 一种轨道转移过程中的姿态确定方法
CN111099040B (zh) * 2019-10-18 2021-10-29 上海航天控制技术研究所 一种基于控制力矩陀螺群控制的系统极性确定方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5100084A (en) * 1990-04-16 1992-03-31 Space Systems/Loral, Inc. Method and apparatus for inclined orbit attitude control for momentum bias spacecraft
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.
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection
US5354016A (en) * 1992-07-30 1994-10-11 General Electric Co. Pivoted wheel roll control with automatic offset
GB9403644D0 (en) * 1994-02-25 1994-04-13 Advanced Robotics Res Manipulator controller
US5875676A (en) * 1997-09-02 1999-03-02 Honeywell Inc. Non colocated rate sensing for control moment gyroscopes

Also Published As

Publication number Publication date
EP1064196B1 (en) 2005-06-08
EP1064196A2 (en) 2001-01-03
JP2002509843A (ja) 2002-04-02
DE69925719D1 (de) 2005-07-14
WO1999050144A2 (en) 1999-10-07
JP4249902B2 (ja) 2009-04-08
US6047927A (en) 2000-04-11
WO1999050144A3 (en) 1999-11-18

Similar Documents

Publication Publication Date Title
DE69925719T2 (de) Singularitätsvermeidung in einer cmg satellitenlageregelung
DE69921790T2 (de) Robuste singularitätsvermeidung in einer satellitenlageregelung
DE69911184T2 (de) Ständige raumfahrzeugslageregelung, wobei singularitätszustände bei der kontrollmomentumsgyroanordnung vermieden werden
DE60120363T2 (de) Orientationsbestimmung in einem neigbaren körper mittels einer modifizierten quaternionsdatendarstellung
EP0856784B1 (de) Verfahren und Vorrichtung zur bordautonomen Bestimmung der Position eines Satelliten
DE69606275T2 (de) Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges
DE69707327T2 (de) Einachsige Korrektur für Bahnneigung
DE69602798T2 (de) Satelliten Drallstabilisationsverfahren, in dem ein transversales Trägheitsmoment mit einem einzigen Freiheitsgrad gespeichert wird, und System dazu
DE3241507A1 (de) Steuersystem fuer eine magnetische lagereinrichtung
JP4249901B2 (ja) 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御
EP3047174B1 (de) Rotationsdämpfer für ein kraftfahrzeug
DE60008103T2 (de) Momenten-positionsregelung
DE3927920A1 (de) Verfahren zur eliminierung von kreiselfehlern
DE3638462A1 (de) Nutationsdaempfeinrichtung fuer doppeldrallraumfahrzeuge
EP0772108B1 (en) Spacecraft attitude or orientation system and method
DE69829529T2 (de) Stabilisierung der Rotationsachse eines Raumfahrzeuges mittels kinetische Energie speichernden Geräten
DE60006120T2 (de) Verbessertes strömungsabriss- und rückgewinnungssteuerungssystem
DE60300944T2 (de) Trägheitsreferenzsystem für ein raumfahrzeug
DE3886714T2 (de) Nutationsensor und nutationsteuerungssystem für einen stabilisierten doppelspinsatellit.
EP0106066A2 (de) Gerät zur Bestimmung der Nordrichtung
DE2150734A1 (de) Steuerungssystem fuer Richtungseinstellung
DE1481508C (de) Verfahren zur Regelung der Querbe" schleunigung und Rolldämpfung von lenkbaren Plugkörpern und Einrichtung zur Durchführung des Verfahrens
DE19543047A1 (de) Vorrichtung zur Erzeugung optimaler Querbeschleunigungen bei zielverfolgenden Flugkörper
JPH02175398A (ja) 人工衛星搭載用視覚センサの指向制御装置

Legal Events

Date Code Title Description
8364 No opposition during term of opposition