FR2710314B1 - Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. - Google Patents

Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe.

Info

Publication number
FR2710314B1
FR2710314B1 FR9311340A FR9311340A FR2710314B1 FR 2710314 B1 FR2710314 B1 FR 2710314B1 FR 9311340 A FR9311340 A FR 9311340A FR 9311340 A FR9311340 A FR 9311340A FR 2710314 B1 FR2710314 B1 FR 2710314B1
Authority
FR
France
Prior art keywords
axis
orientable
solar generator
low orbit
stabilized satellite
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
FR9311340A
Other languages
English (en)
Other versions
FR2710314A1 (fr
Inventor
Philippe Bertheux
Jerome Jarlier
Guy Darmon
Muet Sylvain Le
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9311340A priority Critical patent/FR2710314B1/fr
Priority to US08/306,601 priority patent/US5653407A/en
Priority to GB9419065A priority patent/GB2282114B/en
Priority to DE4434109A priority patent/DE4434109B4/de
Publication of FR2710314A1 publication Critical patent/FR2710314A1/fr
Application granted granted Critical
Publication of FR2710314B1 publication Critical patent/FR2710314B1/fr
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
    • 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
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
FR9311340A 1993-09-23 1993-09-23 Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. Expired - Fee Related FR2710314B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9311340A FR2710314B1 (fr) 1993-09-23 1993-09-23 Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe.
US08/306,601 US5653407A (en) 1993-09-23 1994-09-15 Geocentric pointing three-axis stabilised satellite in low orbit with single-axis steerable solar generator
GB9419065A GB2282114B (en) 1993-09-23 1994-09-20 Satellite
DE4434109A DE4434109B4 (de) 1993-09-23 1994-09-23 Dreiachsenstabilisierter Satellit mit geozentrischer Ausrichtung auf niedrigem Orbit mit einachsenschwenkbarem Solargenerator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9311340A FR2710314B1 (fr) 1993-09-23 1993-09-23 Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe.

Publications (2)

Publication Number Publication Date
FR2710314A1 FR2710314A1 (fr) 1995-03-31
FR2710314B1 true FR2710314B1 (fr) 1995-12-15

Family

ID=9451163

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9311340A Expired - Fee Related FR2710314B1 (fr) 1993-09-23 1993-09-23 Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe.

Country Status (4)

Country Link
US (1) US5653407A (fr)
DE (1) DE4434109B4 (fr)
FR (1) FR2710314B1 (fr)
GB (1) GB2282114B (fr)

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GB2320232B (en) * 1996-12-12 2000-09-27 Ico Services Ltd Satellite and Method of Operating a Satellite
FR2761116B1 (fr) * 1997-03-18 1999-06-04 Matra Marconi Space France Actionneur rotatif a barreau en alliage a memoire de forme
US6076773A (en) * 1998-04-10 2000-06-20 Hughes Electronics Corporation Spin-stabilized spacecraft and methods
WO2000011415A2 (fr) * 1998-08-19 2000-03-02 Mobile Communications Holdings, Inc. Reseau solaire a position adaptative
US6478261B2 (en) * 1998-11-02 2002-11-12 Trw Inc. Spacecraft with deployable panel array
FR2789653B1 (fr) 1999-02-16 2001-04-13 Matra Marconi Space France Satellite a generateur solaire sur bras depliable et procede de mise a poste d'un tel satellite
US7665695B2 (en) * 2003-12-03 2010-02-23 The Boeing Company Unified attitude control for spacecraft transfer orbit operations
US20050133670A1 (en) * 2003-12-03 2005-06-23 Wang H. G. Unified sensor-based attitude determination and control for spacecraft operations
FR2932163B1 (fr) * 2008-06-09 2010-06-11 Astrium Sas Procede de commande d'attitude de satellite et satellite commande en attitude
RU2509694C1 (ru) * 2012-11-28 2014-03-20 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ управления ориентацией солнечной батареи космического аппарата с ограничением угла поворота солнечной батареи
RU2509693C1 (ru) * 2012-11-28 2014-03-20 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ управления ориентацией солнечной батареи космического аппарата с контролем направления вращения и непрерывности изменения информации углового положения солнечной батареи
RU2509692C1 (ru) * 2012-11-28 2014-03-20 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ управления ориентацией солнечной батареи космического аппарата с защитой от кратковременных сбоев информации об угловом положении солнечной батареи
RU2535963C2 (ru) * 2013-02-13 2014-12-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления орбитальным космическим аппаратом
RU2536765C2 (ru) * 2013-02-13 2014-12-27 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления орбитальным космическим аппаратом
RU2544021C2 (ru) * 2013-02-25 2015-03-10 Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Способ ориентации искусственного спутника земли
US10618678B1 (en) * 2015-10-20 2020-04-14 Space Systems/Loral, Llc Self-balancing solar array
CN105539880B (zh) * 2016-01-13 2017-10-13 广西大学 一种大面积可展太阳能翻板
US10368251B1 (en) * 2016-07-25 2019-07-30 SpaceWorks Enterprises, Inc. Satellites and satellite-based systems for ground-to-space short-burst data communications
RU2684241C1 (ru) * 2018-04-05 2019-04-04 Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королёва" Способ управления космическим аппаратом с имеющими одну степень свободы солнечными батареями
FR3105461B1 (fr) * 2019-12-24 2021-12-24 Airbus Defence & Space Sas Procédé de contrôle de l’argument de latitude d’un satellite
CN114084379B (zh) * 2021-11-10 2023-06-23 长光卫星技术股份有限公司 一种摆动式单轴sada控制方法
CN116674769B (zh) * 2023-06-08 2024-01-30 重庆开拓卫星科技有限公司 一种太阳翼多自由度驱动装置

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US4076191A (en) * 1975-04-29 1978-02-28 Rca Corporation Spacecraft component rotation means
US4133501A (en) * 1975-09-30 1979-01-09 Communications Satellite Corporation Self-deployable solar cell panel
US4305555A (en) * 1977-10-20 1981-12-15 Davis Charles E Solar energy system with relay satellite
US4371135A (en) * 1979-07-30 1983-02-01 Rca Corporation Solar array spacecraft reflector
GB2056392B (en) * 1979-08-22 1983-08-03 Rca Corp Attitude control system for spacecraft utilizing the thruster plume
FR2522614A1 (fr) * 1982-03-02 1983-09-09 Centre Nat Etd Spatiales Configuration de satellite a orbite equatoriale a moyens solaires perfectionnes
US4759517A (en) * 1982-06-25 1988-07-26 General Electric Company Station-keeping using solar sailing
US4728061A (en) * 1985-03-20 1988-03-01 Space Industries, Inc. Spacecraft operable in two alternative flight modes
FR2580582B1 (fr) * 1985-04-19 1987-06-26 Matra Procede et dispositif d'amortissement de nutation de satellite par commande d'orientation de masses presentant un produit d'inertie variable
US4830097A (en) * 1987-07-15 1989-05-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Space vehicle thermal rejection system
DE3729389A1 (de) * 1987-09-03 1989-03-16 Messerschmitt Boelkow Blohm Reakquisitionsverfahren fuer die nicklage eines erdsatelliten
US4843294A (en) * 1987-12-01 1989-06-27 Ford Aerospace & Communications Corporation Solar array stepping to minimize array excitation
JPH01237296A (ja) * 1988-03-18 1989-09-21 Mitsubishi Electric Corp 太陽電地パドル装置
JPH0234899A (ja) * 1988-07-23 1990-02-05 Takeshi Harada 電子オルゴール

Also Published As

Publication number Publication date
US5653407A (en) 1997-08-05
GB9419065D0 (en) 1994-11-09
GB2282114B (en) 1997-04-16
GB2282114A (en) 1995-03-29
FR2710314A1 (fr) 1995-03-31
DE4434109B4 (de) 2005-11-10
DE4434109A1 (de) 1995-03-30

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Effective date: 20110531