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Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/26
  • B64G-001/24
  • F03H-001/00
출원번호 US-0875276 (1992-04-28)
발명자 / 주소
  • Tilley Scott W. (Belmont CA) Liu Tung Y. (Union City CA) Higham John S. (Mountain View CA)
출원인 / 주소
  • Space Systems/Loral (Palo Alto CA 02)
인용정보 피인용 횟수 : 45  인용 특허 : 0

초록

A spacecraft (201) maintains its north-south positioning by using one of two pairs of single-gimballed throttled thrusters (221-224) on a face of the spacecraft (201). The throttles (118) and gimbals (116) of the thrusters (221-224) are controlled to produce torques on the spacecraft (201) that will

대표청구항

A wholly-autonomous closed-loop method of simultaneously moving a three-axis stabilized spacecraft having thruster means to attain a desired attitude during north/south maneuvers, said method comprising the steps of: sensing a current spacecraft attitude; determining a first set of forces necessary

이 특허를 인용한 특허 (45)

  1. William A. Hoskins ; Robert J. Cassady, ARC discharge initiation for a pulsed plasma thruster.
  2. Villaume, Fabrice, Active pitch control method and device for an aircraft.
  3. Thomas, Ronald Shawn; Milford, Richard I., Algorithm for simultaneous attitude maneuver and momentum dumping.
  4. Weigl, Harald J.; Goodzeit, Neil E.; Ratan, Santosh, Attitude determination system for yaw-steering spacecraft.
  5. Price Xen ; Chan Kam, Autonomous solar torque management.
  6. Price Xen ; Chan Kam ; Stoen Jeffery, Autonomous spacecraft payload base motion estimation and correction.
  7. Tilley Scott W ; Stratemeier Darren R, Combined stationkeeping and momentum management.
  8. Weiss, Avishai; Di Cairano, Stefano; Walsh, Alex, Concurrent station keeping, attitude control, and momentum management of spacecraft.
  9. John S. Higham ; Keith Reckdahl, Controller and control method for satellite orbit-keeping maneuvers.
  10. Kellberg,Christian J., Deployable spacecraft mount for electric propulsion.
  11. Schroeder Wayne K., Dual-control scheme for improved missile maneuverability.
  12. Goodzeit,Neil Evan; Lempke,James Donald, Efficient orbit sparing system for space vehicle constellations.
  13. Goodzeit, Neil Evan, Fault tolerant attitude control system for zero momentum spacecraft.
  14. Glogowski, Michael Joseph; Goodzeit, Neil Evan, Gimbaled ion thruster arrangement for high efficiency stationkeeping.
  15. Neil Evan Goodzeit ; Santosh Ratan, Gimbaled thruster control system.
  16. Glogowski, Michael; Austin, Philip; Bruno, Dominick; Lentati, Andre, Maneuvering system for earth orbiting satellites with electric thrusters.
  17. Anzel Bernard M., Method and apparatus for a satellite station keeping.
  18. Schroeder Wayne K., Method and apparatus for rapidly turning a vehicle in a fluid medium.
  19. Zentgraf,Peter, Method and system for balancing thrust demands.
  20. Dargent, Thierry, Method and system for stationing a satellite.
  21. Stoen Jeffery D ; Chan Kam, Method to reorient a spacecraft using only initial single axis attitude knowledge.
  22. Stoen Jeffery D ; Chan Kam, Method to reorient a spacecraft using only initial single axis attitude knowledge.
  23. Liu Tung Y ; Chan Kam K, Method using double thruster firings to deadbeat flexible solar array structural oscillations.
  24. Weiss, Avishai; Di Cairano, Stefano; Kalabic, Uros, Model predictive control of spacecraft.
  25. Keitel Keith F. ; Noyola Richard A. ; Yocum ; Jr. John F. ; Abernethy David K. ; Anzel Bernard M., Momentum unloading using gimbaled thrusters.
  26. Hosick Daryl K. ; Gelon Walter S. ; Mills Richard M., Multiple usage thruster mounting configuration.
  27. Kamel Ahmed A. ; Gelon Walter ; Reckdahl Keith, Practical method and apparatus for satellite stationkeeping.
  28. Gelon,Walter; Kamel,Ahmed; Stratemeier,Darren; Hur Diaz,Sun, Practical orbit raising system and method for geosynchronous satellites.
  29. Gnemmi,Patrick; Charon,Romain; Samirant,Michel, Projectile steering by plasma discharge.
  30. Celerier, Bruno, Propulsion system for controlling the orbit and controlling the attitude of a satellite.
  31. Celerier, Bruno, Propulsion system with four modules for satellite orbit control and attitude control.
  32. Kamel Ahmed A ; Ong Kwok M, Satellite camera attitude determination and image navigation by means of earth edge and landmark measurement.
  33. Munir, Saghir; Stratemeier, Darren; Price, Xen; Azziz, Yassir; Delgado, Jorge; Jacinto, Justo, Satellite orbit raising using electric propulsion.
  34. Biber Klaus W., Solar array-mounted stationkeeping and maneuvering thrusters.
  35. Quartararo Richard, Spacecraft attitude control with gimbaled thrusters.
  36. Hans Joerg Koenigsmann, Spacecraft magnetic torquer feedback system.
  37. Woo, Byoungsam; Munir, Mohammad Saghir; Chan, Kam K., Spacecraft momentum management.
  38. Kurland Jeffrey A., Spacecraft momentum management system.
  39. Woo, Byoungsam; Ganji, Farid; Cooper, John Hutton, Spacecraft momentum unload and station-keeping techniques.
  40. Higham, John; Tilley, Scott, Spacecraft transfer orbit techniques.
  41. Fowell, Richard A., System for counteracting a disturbance in a spacecraft.
  42. Goodzeit, Neil E., System for geosynchronous spacecraft rapid earth reacquisition.
  43. Goodzeit, Neil E.; Weigl, Harald J., System for on-orbit correction of spacecraft payload pointing errors.
  44. Munir, Mohammad Saghir; Gelon, Walter; Stratemeier, Darren, Thruster support mechanism for satellite propulsion.
  45. Wang, H. Grant; Li, Rongsheng, Unified attitude control for spacecraft transfer orbit operations.
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