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
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
-
- 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
- B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
- B64G1/2222—Folding
- B64G1/2224—Folding about multiple axes
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Photovoltaic Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2742243B1 (fr) * | 1995-12-06 | 1998-02-13 | Matra Marconi Space France | Procede de commande d'attitude d'un satellite en orbite basse, a acquisition solaire |
US5934620A (en) * | 1996-03-04 | 1999-08-10 | Abernethy; David K. | Spacecraft sun-target steering about an arbitrary body axis |
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 |
US6227497B1 (en) * | 1998-08-19 | 2001-05-08 | Mobile Communications Holdings, Inc. | Adaptively positioned solar array |
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 |
RU2536765C2 (ru) * | 2013-02-13 | 2014-12-27 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Способ управления орбитальным космическим аппаратом |
RU2535963C2 (ru) * | 2013-02-13 | 2014-12-20 | 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 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3817477A (en) * | 1971-07-06 | 1974-06-18 | Trw Inc | Deployable annular solar array |
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 |
-
1993
- 1993-09-23 FR FR9311340A patent/FR2710314B1/fr not_active Expired - Fee Related
-
1994
- 1994-09-15 US US08/306,601 patent/US5653407A/en not_active Expired - Lifetime
- 1994-09-20 GB GB9419065A patent/GB2282114B/en not_active Expired - Fee Related
- 1994-09-23 DE DE4434109A patent/DE4434109B4/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB9419065D0 (en) | 1994-11-09 |
DE4434109A1 (de) | 1995-03-30 |
FR2710314A1 (fr) | 1995-03-31 |
US5653407A (en) | 1997-08-05 |
GB2282114A (en) | 1995-03-29 |
GB2282114B (en) | 1997-04-16 |
DE4434109B4 (de) | 2005-11-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2710314B1 (fr) | Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. | |
GB2226999B (en) | Spacecraft with increased stationkeeping fuel load | |
NO934174D0 (no) | Taksystem som benytter en solcelle | |
IL138421A0 (en) | A retractable thin film solar concentrator for spacecraft | |
DE69427216D1 (de) | Satellitentelekommunikation- und Fernmessanordnung, die sonnensynchrone elliptische Umlaufbahnen mit kurzen Perioden benutzt | |
FI941639A (fi) | Kattopaneli, jossa on aurinkokennosto, sekä kattopanelirakenne, jossa on aurinkokenno | |
DE69229179D1 (de) | Rundfunksysteme und -verfahren, mit zwei preisgünstigen geostationären satelliten | |
DE69627280D1 (de) | Raumfahrzeug mit grossen Ost-West-Ausmassen | |
EP0666602A3 (fr) | Cellule solaire et procédé de fabrication. | |
DE69401189D1 (de) | Geostationärer Satellit mit elektrischen Akkumulatorenzellen | |
DE69400921D1 (de) | Satellit mit aerodynamischer steuereinrichtung | |
SG48549A1 (en) | Diffusion cell | |
EP0618411A3 (fr) | Collecteur solaire. | |
GB2315601B (en) | Antenna structure with active modules | |
Harrap | Stratigraphy and structure of the Monashee terrane in the Mount English area, west of Revelstoke, BC | |
Nataraju et al. | Some special features of INSAT-2 deployment mechanism elements | |
EP0604801A3 (fr) | Cellule solaire à hétérojonction à couches minces. | |
Seidelmann | The International Celestial Reference System | |
Elms | Solar arrays for space station and platforms | |
SINGER | Project SPACE(Solar Power and Climate Equalizer)- SPS used for global climate modifications | |
Hasegawa | Predictions of radiants associated with minor planets. | |
FR2701762B1 (fr) | Dispositif de restitution d'orbite de corps célestes, notamment de satellites artificiels, par écartométrie. | |
REGISTER | Have factory, will launch | |
Buelow | The year of BREM-SAT | |
Gangale | Mare chromium- A short history of Martian timekeeping |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20110531 |