FR2742122B1 - METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS - Google Patents

METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS

Info

Publication number
FR2742122B1
FR2742122B1 FR9514416A FR9514416A FR2742122B1 FR 2742122 B1 FR2742122 B1 FR 2742122B1 FR 9514416 A FR9514416 A FR 9514416A FR 9514416 A FR9514416 A FR 9514416A FR 2742122 B1 FR2742122 B1 FR 2742122B1
Authority
FR
France
Prior art keywords
satellite
solar generators
controlling attitude
attitude
controlling
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
FR9514416A
Other languages
French (fr)
Other versions
FR2742122A1 (en
Inventor
Patrice Damilano
Charles Dagras
Christophe Durteste
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.)
Matra Marconi Space France SA
Original Assignee
Matra Marconi Space France SA
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 Matra Marconi Space France SA filed Critical Matra Marconi Space France SA
Priority to FR9514416A priority Critical patent/FR2742122B1/en
Publication of FR2742122A1 publication Critical patent/FR2742122A1/en
Application granted granted Critical
Publication of FR2742122B1 publication Critical patent/FR2742122B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244Spacecraft control systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR9514416A 1995-12-06 1995-12-06 METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS Expired - Lifetime FR2742122B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9514416A FR2742122B1 (en) 1995-12-06 1995-12-06 METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9514416A FR2742122B1 (en) 1995-12-06 1995-12-06 METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS

Publications (2)

Publication Number Publication Date
FR2742122A1 FR2742122A1 (en) 1997-06-13
FR2742122B1 true FR2742122B1 (en) 1998-02-06

Family

ID=9485193

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9514416A Expired - Lifetime FR2742122B1 (en) 1995-12-06 1995-12-06 METHOD AND DEVICE FOR CONTROLLING ATTITUDE OF SATELLITE WITH SOLAR GENERATORS

Country Status (1)

Country Link
FR (1) FR2742122B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102700728B (en) * 2012-06-18 2014-08-13 上海卫星工程研究所 Method for determining sheltering of solar cell array during in-orbit running of satellite and application of method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3863870A (en) * 1972-07-10 1975-02-04 Hughes Aircraft Co Spin stabilized vehicle and solar cell arrangement therefor
FR2630398B1 (en) * 1988-04-26 1990-08-24 Aerospatiale METHOD FOR TILTING THE MOMENT OF INERTIA OF A FREE ROTATING BODY IN SPACE UNTIL A GIVEN DIRECTION
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection

Also Published As

Publication number Publication date
FR2742122A1 (en) 1997-06-13

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