DE69813663D1 - Einrichtung und Verfahren zum Richten von Sonnenzellenmodulen auf einem agilen, rotierenden Raumfahrzeug - Google Patents

Einrichtung und Verfahren zum Richten von Sonnenzellenmodulen auf einem agilen, rotierenden Raumfahrzeug

Info

Publication number
DE69813663D1
DE69813663D1 DE69813663T DE69813663T DE69813663D1 DE 69813663 D1 DE69813663 D1 DE 69813663D1 DE 69813663 T DE69813663 T DE 69813663T DE 69813663 T DE69813663 T DE 69813663T DE 69813663 D1 DE69813663 D1 DE 69813663D1
Authority
DE
Germany
Prior art keywords
agile
straightening
solar cell
cell modules
rotating spacecraft
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
DE69813663T
Other languages
English (en)
Other versions
DE69813663T2 (de
Inventor
Christopher M Cosner
Scott M Matsunami
David L Behrin
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics 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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69813663D1 publication Critical patent/DE69813663D1/de
Publication of DE69813663T2 publication Critical patent/DE69813663T2/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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • 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
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • 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
    • B64G1/443—Photovoltaic cell 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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
DE69813663T 1997-05-14 1998-05-14 Einrichtung und Verfahren zum Richten von Sonnenzellenmodulen auf einem agilen, rotierenden Raumfahrzeug Expired - Lifetime DE69813663T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/855,684 US6068218A (en) 1997-05-14 1997-05-14 Agile, spinning spacecraft with sun-steerable solar cell array and method
US855684 1997-05-14

Publications (2)

Publication Number Publication Date
DE69813663D1 true DE69813663D1 (de) 2003-05-28
DE69813663T2 DE69813663T2 (de) 2004-02-19

Family

ID=25321843

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69813663T Expired - Lifetime DE69813663T2 (de) 1997-05-14 1998-05-14 Einrichtung und Verfahren zum Richten von Sonnenzellenmodulen auf einem agilen, rotierenden Raumfahrzeug

Country Status (3)

Country Link
US (1) US6068218A (de)
EP (1) EP0878396B1 (de)
DE (1) DE69813663T2 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6463365B1 (en) 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft
US6381520B1 (en) * 2000-07-10 2002-04-30 Space Systems/Loral, Inc. Sun seeking solar array control system and method
JP3488231B1 (ja) * 2002-10-16 2004-01-19 クローバー有限会社 おしぼり製造装置
EP1675187B8 (de) * 2004-12-22 2016-08-24 Thales Schicht zur Verhinderung von elektrostatischer Entladung in einer Ausrüstung im Weltraum
US8403270B2 (en) * 2006-09-15 2013-03-26 The Boeing Company Canted solar array and method for using same
US9247598B2 (en) * 2009-01-16 2016-01-26 Mag Instrument, Inc. Portable lighting devices
RU2539266C2 (ru) * 2013-04-17 2015-01-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления ориентацией космического транспортного грузового корабля с неподвижными панелями солнечных батарей при проведении работ в условиях вращательного движения
RU2539271C2 (ru) * 2013-04-17 2015-01-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления ориентацией космического транспортного грузового корабля с неподвижными панелями солнечных батарей при проведении работ в условиях вращательного движения
RU2539068C2 (ru) * 2013-04-17 2015-01-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления ориентацией космического транспортного грузового корабля с неподвижными панелями солнечных батарей при проведении работ в условиях вращательного движения
CN103274060B (zh) * 2013-04-27 2015-04-22 中国空间技术研究院 一种基于日光反射的航天器补能系统
CN105022402B (zh) * 2015-08-20 2017-11-03 哈尔滨工业大学 一种双刚体航天器快速机动的最短时间确定方法
US10005568B2 (en) * 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3714434A (en) * 1967-07-31 1973-01-30 Hughes Aircraft Co Despin control system for a multispin stabilized device
FR2472509A1 (fr) * 1979-12-27 1981-07-03 Organisation Europ Rech Sp Configuration de satellite artificiel permettant un controle d'attitude continu suivant trois axes
FR2476018A1 (fr) * 1980-02-14 1981-08-21 Org Europeene De Rech Configuration de satellites pour mission geostationnaire
US4375878A (en) * 1980-10-28 1983-03-08 Lockheed Missiles & Space Company, Inc. Space satellite with agile payload orientation system
FR2522614A1 (fr) * 1982-03-02 1983-09-09 Centre Nat Etd Spatiales Configuration de satellite a orbite equatoriale a moyens solaires perfectionnes
JPS6022600A (ja) * 1983-07-18 1985-02-05 日本電気株式会社 デスパンプラツトホ−ム型スピン衛星
JPS60148800A (ja) * 1984-01-17 1985-08-06 日本電気株式会社 スピン安定衛星用デイスパン太陽電池装置
US4834325A (en) * 1985-03-20 1989-05-30 Space Industries, Inc. Modular spacecraft system
US4728061A (en) * 1985-03-20 1988-03-01 Space Industries, Inc. Spacecraft operable in two alternative flight modes
US4747567A (en) * 1985-03-20 1988-05-31 Space Industries, Inc. Spacecraft with articulated solar array
US4752884A (en) * 1985-07-18 1988-06-21 Hughes Aircraft Company Precision platform pointing controller for a dual-spin spacecraft
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
JPH01237296A (ja) * 1988-03-18 1989-09-21 Mitsubishi Electric Corp 太陽電地パドル装置
US5067673A (en) * 1990-02-07 1991-11-26 Hughes Aircraft Company Essentially passive method for inverting the orientation of a dual spin spacecraft
US5255878A (en) * 1990-08-03 1993-10-26 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
US5228644A (en) * 1991-05-28 1993-07-20 The United States Of America As Represented By The United States National Aeronautics And Space Administration Solar powered system for a space vehicle
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft

Also Published As

Publication number Publication date
US6068218A (en) 2000-05-30
EP0878396A1 (de) 1998-11-18
DE69813663T2 (de) 2004-02-19
EP0878396B1 (de) 2003-04-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART