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System and method for calibrating inter-star-tracker misalignments in a stellar inertial attitude determination system 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G01C-021/00
  • G06G-007/78
  • B64G-001/24
  • B64G-001/36
  • F02K-001/00
출원번호 US-0625392 (2000-07-26)
발명자 / 주소
  • Li, Rongsheng
  • Wu, Yeong-Wei Andy
  • Hein, Douglas H.
출원인 / 주소
  • Hughes Electronics Corporation
대리인 / 주소
    Gates & Cooper LLP
인용정보 피인용 횟수 : 13  인용 특허 : 24

초록

A method and apparatus for determining star tracker misalignments is disclosed. The method comprises the steps of defining a defining a reference frame for the star tracker assembly according to a boresight of the primary star tracker and a boresight of a second star tracker wherein the boresight of

대표청구항

A method and apparatus for determining star tracker misalignments is disclosed. The method comprises the steps of defining a defining a reference frame for the star tracker assembly according to a boresight of the primary star tracker and a boresight of a second star tracker wherein the boresight of

이 특허에 인용된 특허 (24)

  1. Didinsky Garry ; Wu Yeong-Wei Andy, Attitude determination system and method.
  2. Yoshikawa Shoji,JPX ; Yamada Katsuhiko,JPX ; Sakashita Hiroshi,JPX ; Yonechi Hiroo,JPX, Attitude determination system for artificial satellite.
  3. Didinsky Garry ; Wu Yeong-Wei ; Li Rongsheng ; Nayak Arunkumar ; Hein Douglas, Autonomous attitude acquisition for a stellar inertial attitude determination system.
  4. Gnatjuk Sevastian Dmitrievich,RUX, Autonomous on-board satellite control system.
  5. Maute Alexandre P. A. (Valbonne FRX), Autonomous orbit control method and system for a geostationary satellite.
  6. Wertz James R. (Torrance CA), Autonomous spacecraft navigation system.
  7. Needelman David D., Confused-in-space stellar attitude acquisition using multiple star trackers.
  8. Wu Yeong-Wei Andy ; Didinsky Garry ; Hein Douglas H., Enhanced stellar attitude determination system.
  9. Wu Yeong-Wei A. (Rancho Palos Verdes CA) Hartman David F. (Chatworth CA) Youhanaie Mark (Playa Del Rey CA), FLIR boresight alignment.
  10. Wu Yeong-Wei A. ; Hein Douglas H. ; Didinsky Garry ; Augenstein David L., Method and apparatus for controlling spacecraft attitude with rotational star trackers.
  11. Wiese Gary E., Method and apparatus for correcting infrared search and track system error.
  12. Didinsky Garry ; Wu Yeong-Wei Andy, Method and apparatus for estimating attitude sensor bias in a satellite.
  13. Surauer Michael,DEX ; Fichter Walter,DEX ; Juckenhoefel Oliver,DEX, Method and system for the autonomous on-board determination of the position of a satellite.
  14. Silverstein Seth David ; Ashe Jeffrey Michael ; Kautz Gregory Michael ; Wheeler Frederick Wilson ; Jacomb-Hood Anthony Wykeham, Method for determining orientation and attitude of a satellite- or aircraft-borne phased-array antenna.
  15. Bender Douglas J. (Redondo Beach CA) Parks Thomas R. (Redondo Beach CA) Brozenec Thomas F. (El Segundo CA), Method of attitude determination using earth and star sensors.
  16. Boeinghoff Albert,DEX ; Bruederle Ernst,DEX, Process for identifying an incorrectly measuring sensor in a spacecraft.
  17. Achkar Issam-Maurice (Cannes la Bocca FRX) Renaud Pierre-Yves (Mandelieu FRX) Sghedoni Michel (Cannes FRX) Guillermin Pierre (Nice FRX), Rate gyro calibration method and apparatus for a three-axis stabilized satellite.
  18. Bender Douglas J. (Redondo Beach CA), Spacecraft attitude determination using sun sensor, earth sensor, and space-to-ground link.
  19. Nielson Marlin Craig, Spacecraft boresight calibration filter.
  20. Krishna Ramuhalli, Star scanning method for determining the line of sight of an electro-optical instrument.
  21. Landecker Peter B. (Manhattan Beach CA) Savage Richard C. (Franktown CO), Surveying satellite apparatus.
  22. Li Rongsheng ; Wu Yeong-Wei A. ; Hein Douglas H. ; Didinsky Garry, System and method for correcting star tracker low spatial frequency error in stellar-inertial attitude determination systems.
  23. Abreu Rene (New Fairfield CT), System and method for sensing attitude of a spacecraft with equilized star tracker errors along three orthogonal axes.
  24. Knobbe Edward J. (Huntington Beach CA) Bose Carl L. (Rancho Palos Verdes CA), Two gimbal error averaging astro-inertial navigator.

이 특허를 인용한 특허 (13)

  1. Ih,Che Hang C., Dynamic modeling technique for the deployment of large satellite antennas.
  2. Stokar, Saul; Neustadter, David, Hybrid tracker.
  3. Li, Rongsheng; Ghassemi, Kamran, Integrated global navigation satellite system and inertial navigation system for navigation and tracking.
  4. Reth, Alan D, Method and apparatus for spacecraft gyroscope scale factor calibration.
  5. Strietzel, Roland; Michel, Klaus; Ratzsch, Dietmar, Method for increasing the reliability of sensor systems.
  6. Needelman,David D.; Fowell,Richard A.; Lai,Peter C.; Wu,Yeong Wei A.; Li,Rongsheng, Multiple stayout zones for ground-based bright object exclusion.
  7. Liu, Dan Y.; Chiang, Richard Y., Position-based gyroless control of spacecraft attitude.
  8. Needelman, David D.; Li, Rongsheng; Wu, Yeong-Wei A., Real-time refinement method of spacecraft star tracker alignment estimates.
  9. Needelman,David D.; Li,Rongsheng; Wu,Yeong Wei A., Refinement of spacecraft angular velocity and attitude estimates using star data.
  10. Liu, Dan Y.; Chiang, Richard Y., Spacecraft acquisition maneuvers using position-based gyroless control.
  11. Tsao, Tung-Ching; Chiang, Richard Y., Star tracker rate estimation with kalman filter enhancement.
  12. Wang,H. Grant; Needelman,David D.; Prakash,Arun, Star-tracker-based attitude determination for spinning spacecraft.
  13. Wang, H. Grant; Li, Rongsheng, Unified attitude control for spacecraft transfer orbit operations.
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