DE60322393D1 - Dynamisches Giersteuerungsverfahren für Raumfahrzeuge - Google Patents

Dynamisches Giersteuerungsverfahren für Raumfahrzeuge

Info

Publication number
DE60322393D1
DE60322393D1 DE60322393T DE60322393T DE60322393D1 DE 60322393 D1 DE60322393 D1 DE 60322393D1 DE 60322393 T DE60322393 T DE 60322393T DE 60322393 T DE60322393 T DE 60322393T DE 60322393 D1 DE60322393 D1 DE 60322393D1
Authority
DE
Germany
Prior art keywords
spacecraft
control method
yaw control
dynamic yaw
dynamic
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
DE60322393T
Other languages
English (en)
Inventor
Klaus Dr Ebert
Wilfried Dr Oesterlin
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 DS GmbH
Original Assignee
Astrium GmbH
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 Astrium GmbH filed Critical Astrium GmbH
Application granted granted Critical
Publication of DE60322393D1 publication Critical patent/DE60322393D1/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
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • 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
    • B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
    • B64G1/503—Radiator panels

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)
  • Navigation (AREA)
DE60322393T 2003-10-21 2003-10-21 Dynamisches Giersteuerungsverfahren für Raumfahrzeuge Expired - Lifetime DE60322393D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03024205A EP1526072B1 (de) 2003-10-21 2003-10-21 Dynamisches Giersteuerungsverfahren für Raumfahrzeuge

Publications (1)

Publication Number Publication Date
DE60322393D1 true DE60322393D1 (de) 2008-09-04

Family

ID=34384597

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60322393T Expired - Lifetime DE60322393D1 (de) 2003-10-21 2003-10-21 Dynamisches Giersteuerungsverfahren für Raumfahrzeuge

Country Status (4)

Country Link
US (2) US7143982B2 (de)
EP (1) EP1526072B1 (de)
DE (1) DE60322393D1 (de)
ES (1) ES2311664T3 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2848529B1 (fr) * 2002-12-12 2005-02-25 Astrium Sas Procede de pilotage solaire de vehicule spatial
US7357356B1 (en) * 2005-02-28 2008-04-15 Lockheed Martin Corporation Attitude and antenna steering system for geosynchronous earth orbit (GEO) spacecraft
CN101346604B (zh) * 2006-02-07 2010-10-20 全球定位有限公司 计算具有可变长时间范围的长期轨道和时钟模型
US7823836B2 (en) * 2006-12-04 2010-11-02 The Boeing Company Optimal sun safe attitude for satellite ground tracking
CN104181930B (zh) * 2014-09-02 2017-02-15 上海新跃仪表厂 一种倾斜轨道卫星偏航机动的自主控制方法
CN104267735B (zh) * 2014-09-02 2017-06-06 上海新跃仪表厂 一种倾斜轨道卫星偏航机动时机判断方法
US9745083B2 (en) * 2015-04-01 2017-08-29 Worldvu Satellites Limited Method for thermal stabilization of a communications satellite
CN105253330B (zh) * 2015-10-30 2017-04-05 中国空间技术研究院 一种基于优化的信息融合geo卫星控制系统菜单式设计方法
CN106364702A (zh) * 2016-09-08 2017-02-01 上海卫星工程研究所 适应偏航机动卫星的太阳电池阵控制策略方法
US10175700B2 (en) * 2017-03-22 2019-01-08 The Boeing Company Methods and apparatus to minimize command dynamics of a satellite
CN111208847B (zh) * 2020-01-08 2023-04-28 中国人民解放军国防科技大学 带太阳帆板的倾斜轨道卫星对日最优固定偏航角确定方法
JP7204987B2 (ja) * 2020-02-26 2023-01-16 三菱電機株式会社 軌道姿勢制御装置、人工衛星、軌道姿勢制御方法及びプログラム
CN111861230B (zh) * 2020-07-24 2023-11-28 二十一世纪空间技术应用股份有限公司 一种面向灾害应急的多星协同观测任务规划方法及装置
CN112777003B (zh) * 2020-12-31 2021-09-21 中国人民解放军63923部队 一种防止sada电弧放电对卫星造成损伤的方法及装置
CN114995475B (zh) * 2022-05-13 2024-10-29 上海航天控制技术研究所 一种指向过程中的保测控控制方法
CN115268503B (zh) * 2022-09-28 2023-01-10 中国人民解放军国防科技大学 一种去奇异化的多飞行器三维协同制导方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2729116A1 (fr) * 1995-01-06 1996-07-12 Matra Marconi Space France Procede de commande d'attitude de satellite sur orbite inclinee sur l'equateur terrestre
US5791598A (en) * 1996-01-16 1998-08-11 Globalstar L.P. and Daimler-Benz Aerospace AG Dynamic bias for orbital yaw steering
US6293502B1 (en) * 1998-08-05 2001-09-25 Hughes Electronics Corporation System and method for enhanced solar array pointing in sun-nadir steering
US6164597A (en) * 1999-08-05 2000-12-26 Space Systems/Loral, Inc. Using reflected solar radiation pressure to provide stationkeeping maneuvering of a spacecraft
US6311932B1 (en) * 1999-11-30 2001-11-06 Space Systems/Loral Inc. Yaw steering momentum system
US6470243B1 (en) * 2000-06-30 2002-10-22 Hughes Electronics Corp. Correction of spacecraft steering control law for unexpected orbital inclination effects

Also Published As

Publication number Publication date
ES2311664T3 (es) 2009-02-16
EP1526072B1 (de) 2008-07-23
EP1526072A1 (de) 2005-04-27
US20050103941A1 (en) 2005-05-19
US20070090229A1 (en) 2007-04-26
US7510148B2 (en) 2009-03-31
US7143982B2 (en) 2006-12-05

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