DE60037006D1 - Lageregelung für ein Raumfahrzeug - Google Patents

Lageregelung für ein Raumfahrzeug

Info

Publication number
DE60037006D1
DE60037006D1 DE60037006T DE60037006T DE60037006D1 DE 60037006 D1 DE60037006 D1 DE 60037006D1 DE 60037006 T DE60037006 T DE 60037006T DE 60037006 T DE60037006 T DE 60037006T DE 60037006 D1 DE60037006 D1 DE 60037006D1
Authority
DE
Germany
Prior art keywords
spacecraft
position control
momentum
reaction
reaction means
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
DE60037006T
Other languages
English (en)
Other versions
DE60037006T2 (de
Inventor
Antony Philip Holt
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 Ltd
Original Assignee
EADS Astrium Ltd
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 EADS Astrium Ltd filed Critical EADS Astrium Ltd
Publication of DE60037006D1 publication Critical patent/DE60037006D1/de
Application granted granted Critical
Publication of DE60037006T2 publication Critical patent/DE60037006T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64G1/28—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
    • B64G1/244—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
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors

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)
  • Position Fixing By Use Of Radio Waves (AREA)
DE60037006T 2000-03-07 2000-10-19 Lageregelung für ein Raumfahrzeug Expired - Lifetime DE60037006T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0005405A GB2360099B (en) 2000-03-07 2000-03-07 Attitude control system for a spacecraft
GB0005405 2000-03-07

Publications (2)

Publication Number Publication Date
DE60037006D1 true DE60037006D1 (de) 2007-12-20
DE60037006T2 DE60037006T2 (de) 2008-08-28

Family

ID=9887078

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60037006T Expired - Lifetime DE60037006T2 (de) 2000-03-07 2000-10-19 Lageregelung für ein Raumfahrzeug

Country Status (4)

Country Link
EP (1) EP1134640B1 (de)
AT (1) ATE377785T1 (de)
DE (1) DE60037006T2 (de)
GB (1) GB2360099B (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10342866A1 (de) 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung
FR2975180B1 (fr) * 2011-05-09 2019-05-31 Airbus Defence And Space Sas Dispositif et procede de determination d'attitude d'un satellite et satellite embarquant un tel dispositif.
CN103123487B (zh) * 2011-11-21 2017-08-29 上海航天控制工程研究所 一种航天器姿态确定方法
CN112325886B (zh) * 2020-11-02 2024-02-02 北京航空航天大学 一种基于重力梯度仪和陀螺仪组合的航天器自主定姿系统

Family Cites Families (5)

* 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
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4617634A (en) * 1983-06-28 1986-10-14 Mitsubishi Denki Kabushiki Kaisha Artificial satellite attitude control system
GB8616385D0 (en) * 1986-07-04 1986-08-13 Marconi Space Systems Ltd Satellite attitude control
US5562266A (en) * 1992-10-29 1996-10-08 Aerospatiale Societe Nationale Industrielle Rate gyro calibration method and apparatus for a three-axis stabilized satellite

Also Published As

Publication number Publication date
GB0005405D0 (en) 2000-04-26
EP1134640B1 (de) 2007-11-07
GB2360099A (en) 2001-09-12
ATE377785T1 (de) 2007-11-15
DE60037006T2 (de) 2008-08-28
GB2360099B (en) 2004-02-11
EP1134640A3 (de) 2004-08-11
EP1134640A2 (de) 2001-09-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: ASTRIUM LTD., STEVENAGE, HERTFORDSHIRE, GB