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Single axis correction for orbit inclination

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/28
  • B64G-001/36
출원번호 US-0608238 (1996-02-28)
발명자 / 주소
  • Fowell Richard A.
출원인 / 주소
  • Hughes Electronics
대리인 / 주소
    Gudmestad
인용정보 피인용 횟수 : 24  인용 특허 : 13

초록

A method and system of orienting a payload of an orbiting spacecraft (14) to maintain a desired pointing profile in the presence of orbit inclination. A cone (12) is determined which is traced in inertial space by a pitch axis of the payload to maintain the desired pointing profile throughout an orb

대표청구항

[ What is claimed is:] [1.] A method of orienting a payload of an orbiting spacecraft including a bias momentum storage means to maintain a desired pointing profile other than at Earth center in a presence of orbit inclination, the method comprising the steps of:determining a cone which is traced in

이 특허에 인용된 특허 (13)

  1. Broquet Jean B. (Saint Cyr l\Ecole FRX), Attitude control systems for space vehicles.
  2. Agrawal Brij N. (9 Thorburn Pl. Gaithersburg MD 20878) Madon Pierre J. (1033 - 22nd St. ; N.W. Washington DC 20037), Attitude pointing error correction system and method for geosynchronous satellites.
  3. Brainard Robert E. (Reno NV), Gyro platform assembly with a spinning vehicle.
  4. Rosen Harold A. (Santa Monica CA), High torque double gimbal control moment gyro.
  5. Scheit Arnold (Mnchen DEX) Fischer Horst-Dieter (Unterhaching DEX), Method and a device for aligning a space vehicle, particularly a geostationary satellite, in a reference direction.
  6. Anzel Bernard M. (El Segundo CA), Method and apparatus for a satellite station keeping.
  7. Rahn Christopher D. (Pleasant Hill CA) Lehner John A. (Sunnyvale CA) Gamble Donald W. (Menlo Park CA), Method and apparatus for inclined orbit attitude control for momentum bias spacecraft.
  8. Westerlund Lawrence H. (Rockville MD), Method of orienting a synchronous satellite.
  9. Kishimoto Hitoshi (Yokohama JPX), Orientation control apparatus for space vehicle.
  10. Muhlfelder ; Ludwig, Roll/yaw body steering for momentum biased spacecraft.
  11. Flament Patrick (Le Cannet FRX), Satellite roll and yaw attitude control method.
  12. Savoca Robert C. (Ridgefield CT), Scanning earth sensor using the sun\s position for determining yaw.
  13. Fowell Richard A. (Culver City CA), Two-axis attitude correction for orbit inclination.

이 특허를 인용한 특허 (24)

  1. Weigl, Harald J.; Goodzeit, Neil E.; Ratan, Santosh, Attitude determination system for yaw-steering spacecraft.
  2. Goodzeit,Neil Evan; Lempke,James Donald, Efficient orbit sparing system for space vehicle constellations.
  3. Turner Andrew E. ; Ford David F. ; Stoen Jeffrey D., Equatorial-normal body-stabilized spacecraft and control method for inclined orbit operation.
  4. Goodzeit, Neil Evan, Fault tolerant attitude control system for zero momentum spacecraft.
  5. Fowell Richard A. ; Yocum John F., Gyroscopic calibration methods for spacecraft.
  6. Haber William Joe ; Kroncke George Thomas, Method and apparatus for beam management in a satellite communication system.
  7. Didinsky Garry ; Wu Yeong-Wei Andy, Method and apparatus for estimating attitude sensor bias in a satellite.
  8. Walter Fichter DE; Jorg Flemmig DE; Gunter Lange DE; Mihael Surauer DE, Method and device for determining the position of communication satellites.
  9. Yung,Kar W.; Chang,Donald C. D., Method and system for maximizing satellite constellation coverage.
  10. Anzel, Bernard M.; Ho, Yiu-Hung M., Methods and apparatus for node-synchronous eccentricity control.
  11. Alfred Cellier, Overhead system of inclined eccentric geosynchronous orbiting satellites.
  12. Cellier Alfred, Overhead system of inclined eccentric geosynchronous orbitting satellites.
  13. Anglin, Patrick T.; Bounds, Ronald W.; Croom, Christopher A.; Crawford, Paul W.; Hessler, III, Theodore; Kokkalakis, Michael; Lam, Claudia H., Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits.
  14. Wang,Arthur W., Satellite communication system.
  15. Wang,Arthur W., Satellite communications system.
  16. Taormina, Frank; Chang, Donald C. D.; Yung, Kar W.; Cheng, David C.; Mayfield, William W.; Novak, III, John; Wang, Arthur W., Satellite system and method of deploying same.
  17. Cielaszyk David ; Furumoto Nobi ; Machlis Matthew, Spacecraft yaw pointing for inclined orbits.
  18. Wang,Arthur W., System and method for continuous broadcast service from non-geostationary orbits.
  19. Grover, Piyush, System and method for estimating states of spacecraft in planet-moon environment.
  20. Shaltiel, Rabin; Kahane, Allan, System and method for measurement of angular orientation of aerospace platforms.
  21. Goodzeit, Neil E., System for geosynchronous spacecraft rapid earth reacquisition.
  22. Goodzeit, Neil E.; Weigl, Harald J., System for on-orbit correction of spacecraft payload pointing errors.
  23. Willis, Richard Ernest; McIntyre, Richard Ian; McConnell, Peter Robert Henderson; West, Gerald Alexander, Vehicle sensor calibration for determining vehicle dynamics.
  24. Drake John H., Wave based satellite constellation.
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