FR2679345B1 - Systeme et procede de commande d'attitude de vaisseau spatial. - Google Patents

Systeme et procede de commande d'attitude de vaisseau spatial.

Info

Publication number
FR2679345B1
FR2679345B1 FR929205744A FR9205744A FR2679345B1 FR 2679345 B1 FR2679345 B1 FR 2679345B1 FR 929205744 A FR929205744 A FR 929205744A FR 9205744 A FR9205744 A FR 9205744A FR 2679345 B1 FR2679345 B1 FR 2679345B1
Authority
FR
France
Prior art keywords
control system
attitude control
space vessel
vessel attitude
space
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
FR929205744A
Other languages
English (en)
Other versions
FR2679345A1 (fr
Inventor
Goodzeit Neil Evan
Paluszek Michael Adam
Cohen Walter Jacques
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2679345A1 publication Critical patent/FR2679345A1/fr
Application granted granted Critical
Publication of FR2679345B1 publication Critical patent/FR2679345B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels

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)
FR929205744A 1991-07-19 1992-05-12 Systeme et procede de commande d'attitude de vaisseau spatial. Expired - Fee Related FR2679345B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/732,963 US5201833A (en) 1991-07-19 1991-07-19 Attitude control system with reaction wheel friction compensation

Publications (2)

Publication Number Publication Date
FR2679345A1 FR2679345A1 (fr) 1993-01-22
FR2679345B1 true FR2679345B1 (fr) 1994-07-01

Family

ID=24945627

Family Applications (1)

Application Number Title Priority Date Filing Date
FR929205744A Expired - Fee Related FR2679345B1 (fr) 1991-07-19 1992-05-12 Systeme et procede de commande d'attitude de vaisseau spatial.

Country Status (2)

Country Link
US (1) US5201833A (fr)
FR (1) FR2679345B1 (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
US5582368A (en) * 1995-01-23 1996-12-10 Martin Marietta Corp. Reaction wheel speed observer system
US5931421A (en) * 1995-08-11 1999-08-03 Daimler-Benz Aerospace Ag Arrangement for attitude control and stabilization of a three axes stabilized spacecraft
US5826829A (en) * 1996-07-15 1998-10-27 Space Systems/Loral Inc. Spacecraft control system with a trihedral momentum bias wheel configuration
US6141606A (en) * 1998-07-28 2000-10-31 Space Systems/Loral, Inc. Wheel speed control system for spacecraft with rejection of null space wheel momentum
US6138952A (en) * 1999-06-11 2000-10-31 Space Systems/Loral, Inc. Transient free actuator switching
US6285928B1 (en) 2000-01-06 2001-09-04 Space Systems/Loral, Inc. Onboard attitude control using reaction wheels
FR2821683B1 (fr) * 2001-03-01 2003-06-13 Agence Spatiale Europeenne Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace
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
US6702234B1 (en) 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US6775599B2 (en) * 2002-07-10 2004-08-10 Honeywell International Inc. Multi-function reaction wheel assemblies for controlling spacecraft attitude
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
US8412391B2 (en) * 2007-08-17 2013-04-02 Princeton Satelitte Systems Proximity spacecraft maneuvering
US8918236B2 (en) * 2011-06-24 2014-12-23 Honeywell International Inc. Methods and systems for adjusting attitude using reaction wheels
CN103612254B (zh) * 2013-11-14 2015-12-09 北京交通大学 一种利用惯性轮驱动的载物机器人
CN104898686B (zh) * 2015-06-02 2016-04-27 北京航空航天大学 一种基于反作用轮摩擦特性的抗干扰姿态控制方法
CN104932510B (zh) * 2015-06-04 2016-08-24 北京航空航天大学 一种针对飞轮低速摩擦的挠性航天器姿态控制系统与方法
CN105644810B (zh) * 2016-02-05 2017-09-12 上海微小卫星工程中心 一种开环控制反作用轮转速变化及卸载方法
CN105786008B (zh) * 2016-03-31 2017-09-22 北京航空航天大学 一种针对飞轮饱和及摩擦特性的挠性航天器姿态控制方法
CN105929840B (zh) * 2016-05-30 2017-06-06 北京航空航天大学 一种组合体航天器复合分层抗干扰姿态稳定控制方法
CN108327927B (zh) * 2018-01-17 2020-11-06 浙江大学 基于微小卫星的反作用轮组自适应力矩分配控制方法
DE102018118480A1 (de) * 2018-07-31 2020-02-06 Rockwell Collins Deutschland Gmbh Steuerungssystem und -verfahren zum Regeln einer Drallradeinrichtung zur Stabilisierung eines Raumflugkörpers

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3998409A (en) * 1975-03-11 1976-12-21 Rca Corporation Minimization of spacecraft attitude error due to wheel speed reversal
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
US4260942A (en) * 1978-04-17 1981-04-07 Trw Inc. Failure detection and correction system for redundant control elements
US4892273A (en) * 1988-12-30 1990-01-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Active damping of spacecraft structural appendage vibrations
US5020745A (en) * 1989-12-20 1991-06-04 General Electric Company Reaction wheel fricton compensation using dither
US5020744A (en) * 1990-01-12 1991-06-04 General Electric Company Method for acquiring three-axis earth pointing attitude for an initially spinning spacecraft
US5058835A (en) * 1990-06-11 1991-10-22 General Electric Company Wheel speed management control system for spacecraft
US5047945A (en) * 1990-08-09 1991-09-10 General Electric Company Residual magnetic dipole cancellation system for satellites

Also Published As

Publication number Publication date
FR2679345A1 (fr) 1993-01-22
US5201833A (en) 1993-04-13

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Legal Events

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TP Transmission of property
ST Notification of lapse

Effective date: 20090119