JP4354144B2 - 輸送手段用制御システム - Google Patents

輸送手段用制御システム Download PDF

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Publication number
JP4354144B2
JP4354144B2 JP2001508660A JP2001508660A JP4354144B2 JP 4354144 B2 JP4354144 B2 JP 4354144B2 JP 2001508660 A JP2001508660 A JP 2001508660A JP 2001508660 A JP2001508660 A JP 2001508660A JP 4354144 B2 JP4354144 B2 JP 4354144B2
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JP
Japan
Prior art keywords
pair
momentum
saddle
cmg
spin axis
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 - Fee Related
Application number
JP2001508660A
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English (en)
Japanese (ja)
Other versions
JP2004538439A (ja
JP2004538439A5 (enExample
Inventor
ヘイバーグ，クリストファー・ジェイ
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 International Inc
Original Assignee
Honeywell International 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 International Inc filed Critical Honeywell International Inc
Publication of JP2004538439A publication Critical patent/JP2004538439A/ja
Publication of JP2004538439A5 publication Critical patent/JP2004538439A5/ja
Application granted granted Critical
Publication of JP4354144B2 publication Critical patent/JP4354144B2/ja
Anticipated expiration legal-status Critical
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    • 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)
JP2001508660A 1999-06-28 2000-06-28 輸送手段用制御システム Expired - Fee Related JP4354144B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (3)

Publication Number Publication Date
JP2004538439A JP2004538439A (ja) 2004-12-24
JP2004538439A5 JP2004538439A5 (enExample) 2007-05-10
JP4354144B2 true JP4354144B2 (ja) 2009-10-28

Family

ID=23335015

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001508660A Expired - Fee Related JP4354144B2 (ja) 1999-06-28 2000-06-28 輸送手段用制御システム

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
DE60008103T2 (de) 2004-12-09
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
WO2001002921A2 (en) 2001-01-11
CA2378157A1 (en) 2001-01-11

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