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특허 상세정보

Method for controlling the pitch attitude of a satellite by means of solar radiation pressure and satellite, in particul

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/24   
미국특허분류(USC) 244/168 ; 244/173
출원번호 US-0916153 (1992-07-24)
우선권정보 FR-0015050 (1990-11-30)
국제출원번호 PCT/FR91/00938 (1991-11-26)
§371/§102 date 19920724 (19920724)
국제공개번호 WO-9209479 (1992-06-11)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0

A satellite embodying at least one surface intended mainly for exposure to solar radiation and extending away from the satellite in a predetermined direction (Y), an on-board computer having connected thereto an attitude sensing system, an orbit control system for imparting thrust to the satellite along predetermined axes, and an attitude control system. The satellite further embodies a device for controlling the tilt of the surface in parallel with a plurality of planes containing the predetermined direction; and, therefore, particularly in parallel wit...


An attitude control system for a satellite, said attitude control system comprising: a satellite having attitude stabilizing means for controlling said attitude about a pitch, yaw and roll axis while said satellite is in a geostationary orbit; an onboard computer mounted to said satellite, said attitude stabilizing means being in communication with said onboard computer; at least one surface member extending from said satellite in a first direction away from said satellite, said at least one surface member adapted to be exposed to solar radiation; orbit ...

이 특허를 인용한 특허 피인용횟수: 21

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  3. Randolph, Thomas; Oh, David; Guenter, Fischer. Energy managed electric propulsion methods and systems for stationkeeping satellites. USP2003066581880.
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  5. Wang,Hanching Grant; Fowell,Richard A.; Ih,Che Hang C.. Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector. USP2006016990396.
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  7. Guyot, Francois. Method and system for unloading the inertia wheels of a spacecraft. USP2014088798816.
  8. Bang,Hyo Choog; Kumar,Krishna Dev; Thak,Min Jae. Method for controlling the attitude of an satellites in elliptic orbits using solar radiation pressure. USP2007037185856.
  9. Weiss, Avishai; Di Cairano, Stefano; Kalabic, Uros. Model Predictive control of spacecraft. USP2018019874879.
  10. Hosick Daryl K. ; Gelon Walter S. ; Mills Richard M.. Multiple usage thruster mounting configuration. USP2000036032904.
  11. Doubrere, Patrick. Satellite comprising electrical propulsion means, method for placing such a satellite in a station and method for keeping said satellite in its station. USP2018039926087.
  12. Sullivan John M.. Satellite solar array and method of biasing to reduce seasonal output power fluctuations. USP1999045895014.
  13. Lehner John A. (Sunnyvale CA) Holmes Thomas (Portola Valley CA). Satellite stabilization system. USP1997045618012.
  14. Griffin Steven ; Huybrechts Steven ; Meink Troy ; Das Alok ; Reinhardt Kitt. Solar sail for power generation. USP2001026194790.
  15. Price Xen ; Randolph Thomas ; Chan Kam K. ; Kamel Ahmed. Spacecraft attitude control system using low thrust thrusters. USP2000046053455.
  16. Abernethy David K.. Spacecraft sun-target steering about an arbitrary body axis. USP1999085934620.
  17. Mark A. Blair. Spacecraft sunshield for use in performing solar torque balancing. USP2002116481671.
  18. Caplin Glenn. Spacecraft with large east-west dimensions. USP1998115833175.
  19. Bender Douglas J. ; Nakano William A. ; Burkett William L. ; Obert Kenneth R. ; Bowles Tiffany ; Bockman Stuart F.. Sun-referenced safe-hold control for momentum biased satellites. USP2000026021979.
  20. McClure, Paul D.; Dorsett, Kenneth M.. System and method for desaturation of a control moment gyroscope. USP2013108561944.
  21. Amalric, Joel. Thrust nozzle system and method for the orbit and attitude control of a geostationary satellite. USP2018019878807.