FR2662997B1 - Systeme de commande de gestion de vitesses de volants pour un engin spatial. - Google Patents

Systeme de commande de gestion de vitesses de volants pour un engin spatial.

Info

Publication number
FR2662997B1
FR2662997B1 FR9104158A FR9104158A FR2662997B1 FR 2662997 B1 FR2662997 B1 FR 2662997B1 FR 9104158 A FR9104158 A FR 9104158A FR 9104158 A FR9104158 A FR 9104158A FR 2662997 B1 FR2662997 B1 FR 2662997B1
Authority
FR
France
Prior art keywords
control system
steering wheel
wheel speed
management control
space vehicle
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
FR9104158A
Other languages
English (en)
Other versions
FR2662997A1 (fr
Inventor
Evan Goodzeit Neil
Mark Linder David
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 FR2662997A1 publication Critical patent/FR2662997A1/fr
Application granted granted Critical
Publication of FR2662997B1 publication Critical patent/FR2662997B1/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)
FR9104158A 1990-06-11 1991-04-05 Systeme de commande de gestion de vitesses de volants pour un engin spatial. Expired - Fee Related FR2662997B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/535,675 US5058835A (en) 1990-06-11 1990-06-11 Wheel speed management control system for spacecraft

Publications (2)

Publication Number Publication Date
FR2662997A1 FR2662997A1 (fr) 1991-12-13
FR2662997B1 true FR2662997B1 (fr) 1995-05-24

Family

ID=24135278

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9104158A Expired - Fee Related FR2662997B1 (fr) 1990-06-11 1991-04-05 Systeme de commande de gestion de vitesses de volants pour un engin spatial.

Country Status (2)

Country Link
US (1) US5058835A (fr)
FR (1) FR2662997B1 (fr)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5201833A (en) * 1991-07-19 1993-04-13 General Electric Company Attitude control system with reaction wheel friction compensation
CA2080612A1 (fr) * 1991-11-27 1993-05-28 Douglas J. Bender Methode et dispositif pour compenser les couples de perturbation magnetique dans un satellite
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection
US5608634A (en) * 1992-06-12 1997-03-04 Martin Marietta Corp. Low noise spacecraft body rate sensing arrangement for attitude control
US5452869A (en) * 1992-12-18 1995-09-26 Hughes Aircraft Company On-board three-axes attitude determination and control system
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft
DE69606275T2 (de) * 1995-08-11 2000-07-13 Daimler Chrysler Ag Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges
US5826829A (en) * 1996-07-15 1998-10-27 Space Systems/Loral Inc. Spacecraft control system with a trihedral momentum bias wheel configuration
US6068217A (en) * 1996-10-16 2000-05-30 Space Systems/Loral, Inc. Method to reorient a spacecraft using only initial single axis attitude knowledge
US5935176A (en) * 1996-11-22 1999-08-10 Lockheed Martin Corporation Momentum wheel oscillation filter
US5984237A (en) * 1997-02-13 1999-11-16 Lockheed Martin Corp. Delta-V targeting system for three-axis controlled spacecraft
US6076772A (en) * 1997-12-15 2000-06-20 Hughes Electronics Corporation Methods for controlling spacecraft attitudes without exciting spacecraft resonances
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
US6340137B1 (en) * 1998-08-26 2002-01-22 Honeywell International Inc. Moment control unit for spacecraft attitude control
KR100311736B1 (ko) * 1998-10-12 2002-11-13 한국과학기술원 인공위성제어용모멘텀휠조립체
EP1076005B1 (fr) * 1999-08-13 2007-01-03 Hughes Electronics Corporation Contrôle orbital d'engin spatial à retour de signal de position orbitale
US6285928B1 (en) * 2000-01-06 2001-09-04 Space Systems/Loral, Inc. Onboard attitude control using reaction wheels
US6456907B1 (en) * 2000-01-31 2002-09-24 Space Systems/Loral, Inc. System and method for limiting the effects of actuator saturation to certain body axes of a spacecraft
US6691955B2 (en) * 2001-11-27 2004-02-17 Space Systems/Loral Spacecraft having a momentum wheel configuration that prevents zero wheel speeds
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
US6600976B1 (en) * 2002-03-29 2003-07-29 Lockheed Martin Corporation Gyroless control system for zero-momentum three-axis stabilized spacecraft
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
US6758444B1 (en) * 2002-12-30 2004-07-06 Honeywell International Inc. Momentum control system and method
DE10342866A1 (de) * 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung
US7198232B1 (en) 2004-08-26 2007-04-03 Lockheed Martin Corporation Optimal speed management for reaction wheel control system and method
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
KR100932156B1 (ko) * 2007-12-24 2009-12-16 한국항공우주연구원 영공간 벡터를 이용한 반작용휠 모멘텀 분배 방법
US20090205695A1 (en) * 2008-02-15 2009-08-20 Tempronics, Inc. Energy Conversion Device

Family Cites Families (5)

* 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
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
FR2369612A1 (fr) * 1976-10-27 1978-05-26 Matra Perfectionnements aux dispositifs de commande d'attitude pour vehicules
FR2423808A1 (fr) * 1978-04-18 1979-11-16 Matra Perfectionnements aux procedes et dispositifs de commande d'attitude et de stockage d'energie pour vehicule spatial
JPH07102839B2 (ja) * 1988-07-05 1995-11-08 三菱電機株式会社 宇宙飛翔体のホイールによる姿勢制御方法

Also Published As

Publication number Publication date
FR2662997A1 (fr) 1991-12-13
US5058835A (en) 1991-10-22

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse

Effective date: 20081231