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특허 상세정보

Method for controlling the pitch attitude of a satellite by means of solar radiation pressure

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/24   
미국특허분류(USC) 244/168 ; 701/013
출원번호 US-0779509 (1997-01-07)
우선권정보 FR-0015050 (1990-11-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Vanophem Meehan & Vanophem, P. C.
인용정보 피인용 횟수 : 17  인용 특허 : 5

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...


[ What is claimed is:] [1.] A method of controlling the attitude of a satellite relative to a predetermined axis thereof, said satellite comprising:a satellite body;at least one planar surface member exposed to solar radiation pressure, said at least one planar surface member having a central axis extending in a first direction away from said satellite body, said first direction being substantially coaxial with said predetermined axis;an attitude measuring device adapted to measure an attitude error angle about said predetermined axis; anda computer conn...

이 특허를 인용한 특허 피인용횟수: 17

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  2. Yamashita, Toshiaki. Maneuver device for artificial satellite. USP2003096622969.
  3. 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.
  4. Cuilleron, Nicolas; Sperandei, Jean; Laurens, Philippe. Method and device for control of a sunlight acquisition phase of a spacecraft. USP2018069988162.
  5. Zentgraf,Peter. Method and system for balancing thrust demands. USP2006117133815.
  6. Wehner,James W.; Harris,Christian M.; O'Rell,Michael K.. Method for aligning a spacecraft. USP2006057051981.
  7. 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.
  8. Vandenbussche, Francis; Janvier, Michel Philippe; Van Overbeek, Antonius Josephus Maria; Holt, Antony Philip. Method of controlling or stabilizing the attitude of a vehicle in space. USP2003036536713.
  9. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  10. Wehner, James W.; Harris, Christian M.; O'Rell, Michael K.. Solar torque control using thin film directionally reflective, emissive, absorptive and transmissive surfaces. USP2005076921050.
  11. Price Xen ; Randolph Thomas ; Chan Kam K. ; Kamel Ahmed. Spacecraft attitude control system using low thrust thrusters. USP2000046053455.
  12. Wehner,James W.; Harris,Christian M.; O'Rell,Michael K.. Spacecraft including control vanes having variable absorptive, reflective and emissive characteristics. USP2007057219860.
  13. Amalric, Joel. Thrust nozzle system and method for the orbit and attitude control of a geostationary satellite. USP2018019878807.
  14. Jarrell, John A.. Unmanned aerial vehicle communication, monitoring, and traffic management. USP2017069691285.
  15. Jarrell, John A.. Unmanned aerial vehicle communication, monitoring, and traffic management. USP2017029576493.
  16. Jarrell, John A.. Unmanned aerial vehicle communication, monitoring, and traffic management. USP2015079087451.
  17. Jarrell, John A.. Unmanned aerial vehicle communication, monitoring, and traffic management. USP2016109466218.