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Autonomous spacecraft payload base motion estimation and correction 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/24
  • B64G-001/38
  • B64G-001/36
출원번호 US-0935044 (1997-09-22)
발명자 / 주소
  • Price Xen
  • Chan Kam
  • Stoen Jeffery
출원인 / 주소
  • Space Systems/Loral, Inc.
대리인 / 주소
    Perman & Green, LLP
인용정보 피인용 횟수 : 10  인용 특허 : 26

초록

A feedback motion compensation (FMC) component for use in a spacecraft having a payload. The FMC component includes a controller having sensor data inputs and an open loop dynamics model that is driven by actuator commands to produce a high accuracy attitude estimate suitable for payload motion comp

대표청구항

[ What is claimed is:] [1.] A feedback motion compensation (FMC) component for use in a three axis body stabilized spacecraft having a payload, comprising a controller having sensor data inputs and including an open loop dynamics model driven by spacecraft actuator commands to produce a high accurac

이 특허에 인용된 특허 (26)

  1. Wertz James R. (Torrance CA), Autonomous spacecraft navigation system.
  2. Chan Fred N. (Atherton CA) Reimche Wallace E. (Saratoga CA), Autonomous stationkeeping for three-axis stabilized spacecraft.
  3. Schmidt ; Jr. George E. (Vincentown NJ), Closed-loop magnetic roll/yaw control system for high inclination orbit satellites.
  4. Liu Tung Y. (Union City CA) Tilley Scott W. (Belmont CA), Compensated transition for spacecraft attitude control.
  5. Adsit Rhys (Milpitas CA) Liu Tung (Union City CA) Chan Fred N. T. (Atherton CA) Weyandt ; Jr. Charles J. (Yardley PA) Tilley Scott (Belmont CA) Bayloca Michel (Menlo Park CA), Control system and method for spacecraft attitude control.
  6. Chan Fred N. (Atherton CA) Nilsen Frank C. (Mountain View CA), Digital PWPF three axis spacecraft attitude control.
  7. Lehner John A. (Sunnyvale CA) Lebsock Kenneth L. (Manhattan Beach CA), Electronic on-orbit roll/yaw satellite control.
  8. Bird Aneurin G. (Katwijk NLX) van Holtz Leopold C. (Aerdenhout NLX), Fast earth recovery procedure for earth-pointing satellites.
  9. Schmidt ; Jr. ; George Edwin ; Muhlfelder ; Ludwig, Magnetic control of spacecraft roll disturbance torques.
  10. Vorlicek Preston L. (Memphis TN), Method for spinning up a three-axis controlled spacecraft.
  11. Basuthakur Sibnath (Rancho Palos Verde CA) Slafer Loren I. (Los Angeles CA), On-board three-axes attitude determination and control system.
  12. Plescia Carl T. (Sunnyvale CA) Gamble Donald W. (Palo Alto CA), Pointing compensation system for spacecraft instruments.
  13. Wirthman David J. (Mountain View CA) Higham John S. (Mountain View CA) Baylocq Michel B. (Menlo Park CA) Chu Peter Y. (Palo Alto CA), Post transition momentum management.
  14. Slafer Loren I. (Los Angeles CA) Bender Douglas J. (Santa Barbara CA) Yocum John F. (Rancho Palos Verdes CA), Precision platform pointing controller for a dual-spin spacecraft.
  15. Loewenthal Stuart H., Reactionless, momentum compensated payload positioner.
  16. Muhlfelder ; Ludwig, Roll/yaw body steering for momentum biased spacecraft.
  17. Kazimi Fatima (San Carlos CA) White Lisa K. (Menlo Park CA) Plescia Carl T. (Sunnyvale CA), Spacecraft East/West orbit control during a North or South stationkeeping maneuver.
  18. Chu Peter Y. (Palo Alto CA) Tadros Alfred H. (San Jose CA), Spacecraft antenna pointing error correction.
  19. Tilley Scott W. (Belmont CA) Liu Tung Y. (Union City CA) Higham John S. (Mountain View CA), Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters.
  20. Garg Subhash C. (San Jose CA) Bhat Mahabaleshwar K. P. (San Jose CA), Spacecraft attitude control using coupled thrusters.
  21. Hubert Carl H. (East Windsor NJ) Miller Paul A. (Hamilton NJ), Spacecraft stabilization system and method.
  22. Fuldner William V. (Lower Makefield Township ; Morrisville County PA) Ganssle Eugene R. (Skillman NJ), Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages.
  23. Clark John F. (Princeton NJ), Station-keeping using solar sailing.
  24. Smay John W. (Torrance CA), System for autonomous earth-pointing acquisition of a dual-spin satellite.
  25. Garg Subhash C. (San Jose CA) Gretz Bruce D. (Philadelphia PA), Transition control system for spacecraft attitude control.
  26. Fowell Richard A. (Culver City CA), Two-axis attitude correction for orbit inclination.

이 특허를 인용한 특허 (10)

  1. Greenfeld, Israel; Yavin, Zvi; Uhl, Bernd, Airborne reconnaissance system.
  2. Li, Rongsheng; Wu, Yeong-Wei A.; Wang, Hanching Grant, Attitude control methods and systems for multiple-payload spacecraft.
  3. Liu,Ketao; Burch,Justin; Becker,Gregory S.; Nelson,Patrick A., Gimbal disturbance calibration and compenstion.
  4. Kienholz David A., Large airborne stabilization/vibration isolation system.
  5. Yu, Qingbo; Men, Jizhuo; Zhao, Shulun; Lang, Rong; Liu, Xiaobin; Yang, Chunxiang, Method and system for controlling antenna of mobile communication application system based on double quaternions in MEMS inertial navigation.
  6. Covello, James A.; Laracuente, Angel D.; Fretheim, Tormod, Non-causal attitude estimation for real-time motion compensation of sensed images on a moving platform.
  7. Sharma, Manu; Wang, Qinghong W., On-line inertia estimation for use in controlling an aerospace vehicle.
  8. Strength Vernon Edward ; Buser Richard R., Payload control system and payload controller for outer space vehicle payloads.
  9. Fischer, Horst-Dieter; Chemnitz, Joachim, Process for determining the position of a spacecraft with the aid of a directional vector and a total angular momentum measurement.
  10. Sekine Koji,JPX, State control device of moving body and its state control method.
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