DE69617060D1 - Vorrichtung zur Stabilisierung eines Satelliten - Google Patents

Vorrichtung zur Stabilisierung eines Satelliten

Info

Publication number
DE69617060D1
DE69617060D1 DE69617060T DE69617060T DE69617060D1 DE 69617060 D1 DE69617060 D1 DE 69617060D1 DE 69617060 T DE69617060 T DE 69617060T DE 69617060 T DE69617060 T DE 69617060T DE 69617060 D1 DE69617060 D1 DE 69617060D1
Authority
DE
Germany
Prior art keywords
satellite
stabilizing
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
DE69617060T
Other languages
English (en)
Other versions
DE69617060T2 (de
Inventor
John A Lehner
Thomas Holmes
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.)
Maxar Space LLC
Original Assignee
Space Systems Loral LLC
Loral Space Systems Inc
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 Space Systems Loral LLC, Loral Space Systems Inc filed Critical Space Systems Loral LLC
Publication of DE69617060D1 publication Critical patent/DE69617060D1/de
Application granted granted Critical
Publication of DE69617060T2 publication Critical patent/DE69617060T2/de
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
    • B64G1/42—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
    • B64G1/24—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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Sustainable Development (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Sustainable Energy (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
  • Photovoltaic Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69617060T 1995-01-12 1996-01-11 Vorrichtung zur Stabilisierung eines Satelliten Expired - Fee Related DE69617060T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/371,821 US5618012A (en) 1995-01-12 1995-01-12 Satellite stabilization system

Publications (2)

Publication Number Publication Date
DE69617060D1 true DE69617060D1 (de) 2002-01-03
DE69617060T2 DE69617060T2 (de) 2002-07-18

Family

ID=23465544

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69617060T Expired - Fee Related DE69617060T2 (de) 1995-01-12 1996-01-11 Vorrichtung zur Stabilisierung eines Satelliten

Country Status (5)

Country Link
US (1) US5618012A (de)
EP (1) EP0722133B1 (de)
JP (1) JPH08244694A (de)
CA (1) CA2163281A1 (de)
DE (1) DE69617060T2 (de)

Families Citing this family (15)

* 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
US5775645A (en) * 1996-03-05 1998-07-07 Hughes Electronics Corporation Controlled-emission solar tabs for attitude solar sailing
US5966640A (en) * 1996-12-24 1999-10-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Satellite antenna management system and method
KR20000001836A (ko) * 1998-06-15 2000-01-15 윤종용 인접 주파수를 사용하는 시스템간의 간섭 제거를 위한 반사장치
US6189835B1 (en) * 1999-04-30 2001-02-20 Hughes Electronics Corporation Apparatus for spacecraft angular momentum control through the use of reflective thermal blankets
US6164597A (en) * 1999-08-05 2000-12-26 Space Systems/Loral, Inc. Using reflected solar radiation pressure to provide stationkeeping maneuvering of a spacecraft
US6481671B1 (en) 2000-08-14 2002-11-19 Ball Aerospace & Technologies Corp. Spacecraft sunshield for use in performing solar torque balancing
DE102007052710B4 (de) * 2007-11-06 2011-02-17 Wabco Gmbh Elektropneumatische Bremssteuerungsanordnung für ein Fahrzeug
JP2009269585A (ja) * 2008-05-09 2009-11-19 Yoichi Hanawa 太陽光線遮断人工衛星
FR2980176A1 (fr) * 2011-09-19 2013-03-22 Astrium Sas Procede de controle d'attitude d'un satellite et satellite commande en attitude
WO2013188368A1 (en) * 2012-06-11 2013-12-19 University Of Florida Research Foundation, Inc. Antennas for small satellites
FR3010053B1 (fr) * 2013-08-30 2016-10-21 Thales Sa Procede et dispositif de propulsion electrique de satellite
KR102348398B1 (ko) * 2020-03-11 2022-01-07 인하대학교 산학협력단 궤도 탈출 시스템으로서의 태양광 우주연
CN115077500B (zh) * 2022-05-07 2024-03-29 中国人民解放军国防科技大学 一种地面阳光反射点的确定方法及其相关组件
CN115258204B (zh) * 2022-09-05 2024-04-05 长光卫星技术股份有限公司 一种中低轨通信卫星能源增加方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3116035A (en) * 1959-10-01 1963-12-31 Bell Telephone Labor Inc Attitude control of earth satellites
US3304028A (en) * 1964-08-11 1967-02-14 Hugh L Dryden Attitude control for spacecraft
US3339863A (en) * 1965-09-16 1967-09-05 James E Webb Solar vane actuator
FR2513589A1 (fr) * 1981-09-28 1983-04-01 Aerospatiale Procede et dispositif pour aligner l'axe de roulis d'un satellite avec une direction desiree
FR2522614A1 (fr) * 1982-03-02 1983-09-09 Centre Nat Etd Spatiales Configuration de satellite a orbite equatoriale a moyens solaires perfectionnes
US4684084A (en) * 1984-05-29 1987-08-04 Rca Corporation Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages
WO1990006259A1 (en) * 1988-12-02 1990-06-14 Institut Kosmicheskikh Issledovany Akademii Nauk Sssr Space apparatus
FR2656586B1 (fr) * 1989-12-29 1992-05-07 Aerospatiale Dispositif de controle d'attitude par voiles solaires pour satellite stabilise autour de trois axes.
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
US5305971A (en) * 1992-07-14 1994-04-26 Trw Inc. Spacecraft control by electrochromic devices

Also Published As

Publication number Publication date
EP0722133A2 (de) 1996-07-17
EP0722133B1 (de) 2001-11-21
US5618012A (en) 1997-04-08
DE69617060T2 (de) 2002-07-18
JPH08244694A (ja) 1996-09-24
CA2163281A1 (en) 1996-07-13
EP0722133A3 (de) 1996-12-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee