DE69315129D1 - Verfahren und Vorrichtung zur Momentausgleichung eines Satelliten - Google Patents
Verfahren und Vorrichtung zur Momentausgleichung eines SatellitenInfo
- Publication number
- DE69315129D1 DE69315129D1 DE69315129T DE69315129T DE69315129D1 DE 69315129 D1 DE69315129 D1 DE 69315129D1 DE 69315129 T DE69315129 T DE 69315129T DE 69315129 T DE69315129 T DE 69315129T DE 69315129 D1 DE69315129 D1 DE 69315129D1
- Authority
- DE
- Germany
- Prior art keywords
- satellite
- moment balancing
- balancing
- moment
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/407—Solar sailing
-
- 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
- B64G1/34—Guiding or controlling apparatus, e.g. for attitude control using gravity gradient
-
- 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
-
- 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
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S136/00—Batteries: thermoelectric and photoelectric
- Y10S136/291—Applications
- Y10S136/292—Space - satellite
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Environmental & Geological Engineering (AREA)
- Geology (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Sustainable Energy (AREA)
- Automation & Control Theory (AREA)
- Photovoltaic Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/909,260 US5310144A (en) | 1992-07-06 | 1992-07-06 | Method and apparatus for satellite torque balancing |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69315129D1 true DE69315129D1 (de) | 1997-12-18 |
DE69315129T2 DE69315129T2 (de) | 1998-03-05 |
Family
ID=25426910
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69315129T Expired - Fee Related DE69315129T2 (de) | 1992-07-06 | 1993-07-05 | Verfahren und Vorrichtung zur Momentausgleichung eines Satelliten |
Country Status (4)
Country | Link |
---|---|
US (1) | US5310144A (de) |
EP (1) | EP0578176B1 (de) |
JP (1) | JP2959696B2 (de) |
DE (1) | DE69315129T2 (de) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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. |
US5400987A (en) * | 1993-04-26 | 1995-03-28 | Hughes Aircraft Company | Variable angle latching mechanism for spacecraft |
US5673459A (en) * | 1994-09-28 | 1997-10-07 | Space Systems/Loral, Inc. | Deployment hinge apparatus |
US5669586A (en) * | 1994-12-06 | 1997-09-23 | Space Systems/Loral, Inc. | Satellite gravity gradient compensation using on-orbit solar array reorientation |
FR2732309B1 (fr) * | 1995-03-28 | 1997-06-20 | Centre Nat Etd Spatiales | Dispositif pour l'orientation d'un panneau solaire d'engin spatial et engin ainsi equipe |
FR2738930B1 (fr) * | 1995-09-14 | 1997-11-14 | Matra Marconi Space France | Procede et dispositif passif de pointage d'un engin spatial vers le soleil |
JPH11512677A (ja) * | 1995-10-04 | 1999-11-02 | オーストリアン エアロスペース ゲゼルシャフト ミット ベシュレンクテル ハフツング | 人工衛星構造部材のオリエンテーションを調節する駆動装置 |
AT403030B (de) * | 1995-10-04 | 1997-10-27 | Oesterreichische Raumfahrt Und | Antriebseinrichtung zum verstellen von zu orientierenden bauteilen eines satelliten |
US5816540A (en) * | 1995-12-22 | 1998-10-06 | Hughes Electronics | Optimal solar tracking system |
US5934620A (en) * | 1996-03-04 | 1999-08-10 | Abernethy; David K. | Spacecraft sun-target steering about an arbitrary body axis |
DE19610297C1 (de) * | 1996-03-15 | 1997-01-23 | Daimler Benz Aerospace Ag | Vorrichtung zum Entfalten von zwei Paneelen für Solargeneratoren |
US5906339A (en) * | 1996-11-07 | 1999-05-25 | Motorola, Inc. | Multiple axis solar sailing |
US6003817A (en) * | 1996-11-12 | 1999-12-21 | Motorola, Inc. | Actively controlled thermal panel and method therefor |
FR2765189B1 (fr) * | 1997-06-25 | 1999-08-20 | Agence Spatiale Europeenne | Dispositif de stabilisation passive de la direction de pointage d'un engin spatial |
US6070833A (en) | 1998-04-09 | 2000-06-06 | Hughes Electronics Corporation | Methods for reducing solar array power variations while managing the system influences of operating with off-pointed solar wings |
US6010096A (en) * | 1998-07-22 | 2000-01-04 | Space Systems/Loral, Inc. | Deployment restraint and sequencing device |
US6318675B1 (en) | 1999-10-11 | 2001-11-20 | Hughes Electronics Corporation | Solar wing thermal shock compensation using solar wing position actuator |
AU2001276847A1 (en) * | 2000-06-29 | 2002-01-14 | Honeywell International, Inc. | Method and device for compensating for thermal deformation of a gravity gradientboom on a satellite |
US6481671B1 (en) | 2000-08-14 | 2002-11-19 | Ball Aerospace & Technologies Corp. | Spacecraft sunshield for use in performing solar torque balancing |
US7104506B1 (en) | 2003-08-06 | 2006-09-12 | Lockheed Martin Corporation | Spacecraft disturbance trimming system |
KR100573876B1 (ko) * | 2004-07-13 | 2006-04-25 | 한국과학기술원 | 태양 복사 압력을 이용하여 타원 궤도에 있는 위성 자세제어 방법 |
US20060163434A1 (en) * | 2005-01-27 | 2006-07-27 | Honeywell International Inc., Law Dept. | Spacecraft for interplanetary/lunar travel |
US8352101B2 (en) * | 2009-12-22 | 2013-01-08 | The Boeing Company | Algorithm for simultaneous attitude maneuver and momentum dumping |
US8868263B2 (en) | 2011-05-25 | 2014-10-21 | Space Systems/Loral, Llc | Spacecraft momentum management using solar array |
WO2013013122A1 (en) * | 2011-07-21 | 2013-01-24 | Pro Brand International, Inc. | Snap attachment for reflector mounting |
US20140166815A1 (en) * | 2012-03-12 | 2014-06-19 | Arthur M. Dula | Tether for spacecraft reaction control system |
RU2535979C2 (ru) * | 2012-12-04 | 2014-12-20 | Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Система ориентации навигационного спутника |
US11724836B2 (en) * | 2013-03-15 | 2023-08-15 | Arthur M Dula | Tether for spacecraft reaction control system |
RU2569999C2 (ru) * | 2014-04-29 | 2015-12-10 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Способ ориентации навигационного спутника |
US11009297B2 (en) * | 2015-04-15 | 2021-05-18 | Worldvu Satellites Limited | Fluidicially coupled heat pipes and method therefor |
US10005568B2 (en) | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
US10647450B2 (en) | 2016-03-18 | 2020-05-12 | The Boeing Company | Satellite control system using electrically controllable variable reflection glass panels |
CN112432732B (zh) * | 2020-10-20 | 2022-11-18 | 上海航天控制技术研究所 | 一种自动配平装置及使用方法 |
CN118182875A (zh) * | 2024-05-16 | 2024-06-14 | 哈尔滨工业大学 | 用于平板式卫星的帆板的同步展开设计方法及系统 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304028A (en) * | 1964-08-11 | 1967-02-14 | Hugh L Dryden | Attitude control for spacecraft |
DE2604005A1 (de) * | 1976-02-03 | 1977-08-11 | Messerschmitt Boelkow Blohm | Einrichtung zur beeinflussung der position und lage eines satelliten |
US4325124A (en) * | 1979-02-28 | 1982-04-13 | Organisation Europeenne De Recherches Spatiales | System for controlling the direction of the momentum vector of a geosynchronous satellite |
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 |
DE3329955A1 (de) * | 1983-08-19 | 1985-03-07 | Erno Raumfahrttechnik Gmbh, 2800 Bremen | Lageregelung von satelliten |
US4684084A (en) * | 1984-05-29 | 1987-08-04 | Rca Corporation | Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages |
US4728061A (en) * | 1985-03-20 | 1988-03-01 | Space Industries, Inc. | Spacecraft operable in two alternative flight modes |
US4834325A (en) * | 1985-03-20 | 1989-05-30 | Space Industries, Inc. | Modular spacecraft system |
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 |
FR2615477B1 (fr) * | 1987-05-22 | 1989-08-18 | Centre Nat Etd Spatiales | Dispositif et procede de pointage d'une sonde spatiale vers un corps celeste |
JPH0248299A (ja) * | 1988-08-11 | 1990-02-19 | Mitsubishi Electric Corp | 人工衛星 |
US4949922A (en) * | 1988-12-09 | 1990-08-21 | Hughes Aircraft Company | Satellite control system |
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. |
DE4114804A1 (de) * | 1991-05-07 | 1992-11-12 | Messerschmitt Boelkow Blohm | Vorrichtung zur lageregelung von satelliten mit solardruckmomenten |
-
1992
- 1992-07-06 US US07/909,260 patent/US5310144A/en not_active Expired - Lifetime
-
1993
- 1993-07-05 EP EP93110729A patent/EP0578176B1/de not_active Expired - Lifetime
- 1993-07-05 DE DE69315129T patent/DE69315129T2/de not_active Expired - Fee Related
- 1993-07-06 JP JP5167134A patent/JP2959696B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP2959696B2 (ja) | 1999-10-06 |
DE69315129T2 (de) | 1998-03-05 |
US5310144A (en) | 1994-05-10 |
EP0578176A1 (de) | 1994-01-12 |
EP0578176B1 (de) | 1997-11-12 |
JPH06156397A (ja) | 1994-06-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69315129T2 (de) | Verfahren und Vorrichtung zur Momentausgleichung eines Satelliten | |
DE69319887T2 (de) | Verfahren und vorrichtung zur dynamischen kalibrierung eines differentialodometers | |
DE59308438D1 (de) | Verfahren und Vorrichtung zur Feststellung der Funktionsfähigkeit eines Hämo-Dialysators | |
DE69130850T2 (de) | Verfahren und Vorrichtung zur Weiterübersetzung eines Übersetzungsresultats | |
DE69700728D1 (de) | Verfahren und Vorrichtung zur Lageerhaltung eines Satelliten | |
DE69432447D1 (de) | Verfahren und vorrichtung zur reduktion von störwellen eines kommunikationssystems | |
DE69208345D1 (de) | Verfahren und Vorrichtung zur Sicherung eines Gleiskettengelenks | |
DE69321569D1 (de) | Verfahren und Vorrichtung zur Zeicheneingabe | |
DE59302383D1 (de) | Verfahren und vorrichtung zur ermittlung eines gemischanteils eines gasgemisches | |
DE69432943D1 (de) | Verfahren und Vorrichtung zur Sprachdetektion | |
DE69323966T2 (de) | Verfahren zur Ausführung eines Kopierverfahrens und Vorrichtung zur Durchführung des Verfahrens | |
DE69331756T2 (de) | Verfahren und Vorrichtung zur Erleichterung der Dekoration eines dreidimensionalen Gegenstandes | |
DE69327354T2 (de) | Verfahren und Vorrichtung zum Ziehen von Konturen eines Bildes | |
DE69422845D1 (de) | Vorrichtung und Verfahren zur Koordinateneingabe | |
DE69631277D1 (de) | Verfahren und Vorrichtung zur Landehilfe eines Flügels | |
DE59307383D1 (de) | Verfahren und vorrichtung zur regelung des verzugs eines streckwerks | |
DE69611188D1 (de) | Vorrichtung und Verfahren zur Geschwindigkeitsregelung eines Schiffes | |
DE69616720D1 (de) | Verfahren und Gerät zur Lagemessung eines Satelliten | |
DE69317981D1 (de) | Verfahren und Vorrichtung zur Demontage und Montage eines Artikels | |
DE69317991D1 (de) | Verfahren und Vorrichtung zur Verdichtung eines Gegenstandes | |
DE59307298D1 (de) | Verfahren und Vorrichtung zur Phasenmessung | |
DE69408517D1 (de) | Verfahren und Vorrichtung zur Trennung eines Flüssigkeitsgemisches | |
DE59304872D1 (de) | Vorrichtung und Verfahren zur Lageregelung eines beweglichen Teils | |
DE69611469T2 (de) | Verfahren und Vorrichtung zur Verdampfung eines Flüssigkeitstromes | |
DE69307486D1 (de) | Verfahren und Vorrichtung zur Phasentrennung |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: HUGHES ELECTRONICS CORP., EL SEGUNDO, CALIF., US |
|
8339 | Ceased/non-payment of the annual fee |