DE60008103T2 - Momenten-positionsregelung - Google Patents

Momenten-positionsregelung Download PDF

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Publication number
DE60008103T2
DE60008103T2 DE60008103T DE60008103T DE60008103T2 DE 60008103 T2 DE60008103 T2 DE 60008103T2 DE 60008103 T DE60008103 T DE 60008103T DE 60008103 T DE60008103 T DE 60008103T DE 60008103 T2 DE60008103 T2 DE 60008103T2
Authority
DE
Germany
Prior art keywords
scissors
pair
cmgs
wheel assembly
reaction wheel
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
DE60008103T
Other languages
German (de)
English (en)
Other versions
DE60008103D1 (de
Inventor
J. Christopher HEIBERG
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 DE60008103D1 publication Critical patent/DE60008103D1/de
Publication of DE60008103T2 publication Critical patent/DE60008103T2/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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Vehicle Body Suspensions (AREA)
  • Navigation (AREA)
  • Control Of Position Or Direction (AREA)
  • Operation Control Of Excavators (AREA)
  • Paper (AREA)
  • Body Structure For Vehicles (AREA)
  • Air Bags (AREA)
DE60008103T 1999-06-28 2000-06-28 Momenten-positionsregelung Expired - Lifetime DE60008103T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US340806 1999-06-28
US09/340,806 US6241194B1 (en) 1999-06-28 1999-06-28 Momentum position control
PCT/US2000/017717 WO2001002921A2 (en) 1999-06-28 2000-06-28 Momentum position control

Publications (2)

Publication Number Publication Date
DE60008103D1 DE60008103D1 (de) 2004-03-11
DE60008103T2 true DE60008103T2 (de) 2004-12-09

Family

ID=23335015

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60008103T Expired - Lifetime DE60008103T2 (de) 1999-06-28 2000-06-28 Momenten-positionsregelung

Country Status (8)

Country Link
US (1) US6241194B1 (enExample)
EP (1) EP1188098B1 (enExample)
JP (1) JP4354144B2 (enExample)
AT (1) ATE259078T1 (enExample)
AU (1) AU1324001A (enExample)
CA (1) CA2378157A1 (enExample)
DE (1) DE60008103T2 (enExample)
WO (1) WO2001002921A2 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2796172B1 (fr) * 1999-07-08 2001-09-21 Cit Alcatel Systeme pour le controle d'un satellite en attitude et procede corespondant
US6354163B1 (en) * 2000-05-17 2002-03-12 Honeywell International Inc. Mitigating gimbal induced disturbances in CMG arrays
US6515221B1 (en) * 2000-08-01 2003-02-04 Honeywell International Inc. Modular reaction wheel assembly to shield electronics on a satellite
FR2846107B1 (fr) * 2002-10-21 2005-06-24 Cit Alcatel Dispositif de controle d'attitude d'un satellite geostationnaire
FR2861690B1 (fr) * 2003-11-04 2006-04-07 Eads Astrium Sas Controle d'attitude de satellites en particulier agiles a nombre reduit de gyrodynes
US7014150B2 (en) * 2004-07-30 2006-03-21 Honeywell International Inc. Method and system for optimizing torque in a CMG array
US7627404B2 (en) * 2007-04-13 2009-12-01 The Boeing Company Singularity escape and avoidance using a virtual array rotation
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
US8561944B2 (en) 2010-06-17 2013-10-22 Lockheed Martin Corporation System and method for desaturation of a control moment gyroscope
US20120160965A1 (en) * 2010-12-23 2012-06-28 Muller Ronald M Method to achieve a rapid and low power slew of a satellite
US9745082B2 (en) 2015-06-02 2017-08-29 The Charles Stark Draper Laboratory, Inc. Rapid slew and settle systems for small satellites
US9551994B2 (en) 2015-06-15 2017-01-24 The Boeing Company System and method for vehicle attitude control
US10877158B2 (en) * 2016-12-22 2020-12-29 Myriota Pty Ltd System and method for generating extended satellite ephemeris data

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
DE4129628A1 (de) * 1991-09-06 1993-03-18 Deutsche Aerospace Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges
US5681012A (en) * 1995-01-05 1997-10-28 Hughes Electronics Spacecraft control with skewed control moment gyros
DE19510371C1 (de) * 1995-03-22 1996-10-31 Daimler Benz Aerospace Ag Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit
JP2937123B2 (ja) * 1995-06-15 1999-08-23 日本電気株式会社 宇宙航行体及び宇宙航行体の姿勢制御方法
JPH09226696A (ja) * 1996-02-22 1997-09-02 Toshiba Corp 人工衛星姿勢制御装置
US6053445A (en) * 1996-09-09 2000-04-25 C-1 Design Group Fly fishing reel with isolated conical drag
US6062512A (en) * 1997-08-27 2000-05-16 Hughes Electronics Corporation Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices
US6047927A (en) * 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control

Also Published As

Publication number Publication date
ATE259078T1 (de) 2004-02-15
WO2001002921A3 (en) 2001-07-26
EP1188098B1 (en) 2004-02-04
US6241194B1 (en) 2001-06-05
JP2004538439A (ja) 2004-12-24
DE60008103D1 (de) 2004-03-11
EP1188098A2 (en) 2002-03-20
AU1324001A (en) 2001-01-22
JP4354144B2 (ja) 2009-10-28
WO2001002921A2 (en) 2001-01-11
CA2378157A1 (en) 2001-01-11

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