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GB2121984B - Method of and equipment for adjusting the position of an earth satellite - Google Patents

Method of and equipment for adjusting the position of an earth satellite

Info

Publication number
GB2121984B
GB2121984B GB08310161A GB8310161A GB2121984B GB 2121984 B GB2121984 B GB 2121984B GB 08310161 A GB08310161 A GB 08310161A GB 8310161 A GB8310161 A GB 8310161A GB 2121984 B GB2121984 B GB 2121984B
Authority
GB
United Kingdom
Prior art keywords
adjusting
equipment
earth satellite
satellite
earth
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
Application number
GB08310161A
Other languages
English (en)
Other versions
GB8310161D0 (en
GB2121984A (en
Inventor
Ernst Bruderle
Michio Otsuka
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.)
Airbus Defence and Space GmbH
Mitsubishi Electric Corp
Original Assignee
Messerschmitt Bolkow Blohm AG
Mitsubishi Electric Corp
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 Messerschmitt Bolkow Blohm AG, Mitsubishi Electric Corp filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB8310161D0 publication Critical patent/GB8310161D0/en
Publication of GB2121984A publication Critical patent/GB2121984A/en
Application granted granted Critical
Publication of GB2121984B publication Critical patent/GB2121984B/en
Expired 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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
GB08310161A 1982-04-20 1983-04-14 Method of and equipment for adjusting the position of an earth satellite Expired GB2121984B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823214373 DE3214373A1 (de) 1982-04-20 1982-04-20 Verfahren und einrichtung fuer die lageregelung eines satelliten

Publications (3)

Publication Number Publication Date
GB8310161D0 GB8310161D0 (en) 1983-05-18
GB2121984A GB2121984A (en) 1984-01-04
GB2121984B true GB2121984B (en) 1986-01-29

Family

ID=6161257

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08310161A Expired GB2121984B (en) 1982-04-20 1983-04-14 Method of and equipment for adjusting the position of an earth satellite

Country Status (4)

Country Link
JP (1) JPS58183395A (fr)
DE (1) DE3214373A1 (fr)
FR (1) FR2525359B1 (fr)
GB (1) GB2121984B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108021138A (zh) * 2017-11-03 2018-05-11 西北工业大学 一种地磁场模型简化设计方法

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3606636C1 (de) * 1986-02-28 1987-11-05 Messerschmitt Boelkow Blohm Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system
GB2241480B (en) * 1990-02-28 1993-05-26 British Aerospace Apparatus and method for controlling attitude of a spacecraft orbiting earth or other celestial body
DE4007497A1 (de) * 1990-03-09 1991-09-12 Messerschmitt Boelkow Blohm Vorrichtung zur lageregelung von raumstationen
FR2670745B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite stabilise 3-axes sur orbite a faible inclinaison.
FR2678894B1 (fr) * 1991-07-09 1993-11-19 Aerospatiale Ste Nationale Indle Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu.
CA2080612A1 (fr) * 1991-11-27 1993-05-28 Douglas J. Bender Methode et dispositif pour compenser les couples de perturbation magnetique dans un satellite
FR2718105B1 (fr) * 1994-03-30 1996-06-14 Centre Nat Etd Spatiales Satellite artificiel muni de générateurs de moments magnétiques et aérodynamiques et procédé de commande d'un tel satellite.
FR2724364B1 (fr) * 1994-09-12 1997-01-17 Matra Marconi Space France Procede et systeme de stabilisation selon trois axes d'un satellite d'orbite non-equatoriale
DE19520115A1 (de) * 1995-06-01 1996-12-05 Contraves Gmbh Verfahren zum Bestimmen der Rollage eines rollenden Flugobjektes
JP5595978B2 (ja) * 2011-05-28 2014-09-24 双葉電子工業株式会社 遠隔制御機器の駆動制御装置

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3189298A (en) * 1962-08-06 1965-06-15 Westinghouse Electric Corp Control apparatus for spacecraft
US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
CA1073988A (fr) * 1975-07-21 1980-03-18 Ludwig Muhlfelder Commande de mouvements de roulis et en lacet a boucle fermee de precision pour satellites a orbites a faible inclinaison
US4010921A (en) * 1975-08-20 1977-03-08 The United States Of America As Represented By The Secretary Of The Air Force Spacecraft closed loop three-axis momentum unloading system
JPS5628100A (en) * 1979-08-15 1981-03-19 Mitsubishi Electric Corp Wheel unloading device
JPS56131500A (en) * 1980-03-21 1981-10-15 Mitsubishi Electric Corp Magnetic controlling system for triaxes controlling satellite
US4521855A (en) * 1981-07-27 1985-06-04 Ford Aerospace & Communications Corporation Electronic on-orbit roll/yaw satellite control

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108021138A (zh) * 2017-11-03 2018-05-11 西北工业大学 一种地磁场模型简化设计方法
CN108021138B (zh) * 2017-11-03 2020-05-19 西北工业大学 一种地磁场模型简化设计方法

Also Published As

Publication number Publication date
FR2525359A1 (fr) 1983-10-21
GB8310161D0 (en) 1983-05-18
FR2525359B1 (fr) 1990-03-30
GB2121984A (en) 1984-01-04
JPH0468199B2 (fr) 1992-10-30
DE3214373C2 (fr) 1987-10-15
JPS58183395A (ja) 1983-10-26
DE3214373A1 (de) 1983-10-27

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Effective date: 20030413