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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Momentum biased active three-axis satellite attitude control system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/20   
미국특허분류(USC) 244/165 ; 73/178R ; 244/3.21 ; 244/166 ; 244/171 ; 364/434
출원번호 US-0724577 (1976-09-23)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Norton, Edward J.Christoffersen, H.Lazar, Joseph D.
인용정보 피인용 횟수 : 54  인용 특허 : 1
초록
▼

Control of an active three-axis multiple-wheel attitude control system is provided with a bias momentum to achieve stiffness about the pitch axis. With this stiffness, the system overcomes the inherent inability of a zero momentum system employing the sun as its yaw reference to be provided with this yaw reference during the periods encompassing satellite high noon and midnight (i.e., approximate coalignment of the sun line and the local vertical). The satellite attitude is normally maintained by angular momentum exchange developed by three or more react...

대표청구항이 없습니다

이 특허에 인용된 특허 (1)

  1. Pistiner Josef Siegfried (Lafayette Hill PA). Minimization of spacecraft attitude error due to wheel speed reversal. USP1976123998409.

이 특허를 인용한 특허 피인용횟수: 54

  1. Skutecki Edmund R. (Glendale AZ). Adaptive washout circuit for use in a stability augmentation system. USP1984114481586.
  2. Thomas, Ronald Shawn; Milford, Richard I.. Algorithm for simultaneous attitude maneuver and momentum dumping. USP2013018352101.
  3. Billing-Ross, James A.; Pledger, Douglas B.; Fritz, Teresa A.. Apparatus for determining 3-axis space craft attitude. USP1994065319968.
  4. Bittner Helmut (Munich DEX) Gottzein Eveline (Oberpframmern DEX) Surauer Michael (Chieming DEX). Arrangement for the attitude stabilization of flexible vehicles with weakly-dampened structural vibrations and discontin. USP1986014567564.
  5. Izumida Kiichiro (Kanagawa JPX) Kasai Ritaroh (Kanagawa JPX). Artificial satellite attitude control system. USP1986104617634.
  6. Broquet Jean B. (Saint Cyr l\Ecole FRX). Attitude control systems for space vehicles. USP1981104294420.
  7. Weigl, Harald J.; Goodzeit, Neil E.; Ratan, Santosh. Attitude determination system for yaw-steering spacecraft. USP2010117835826.
  8. 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. USP1990034911385.
  9. Pistiner Josef S. (Lafayette Hill PA). Closed loop roll control for momentum biased satellites. USP1980104230294.
  10. Parks Thomas R. ; Smay John W. ; Harrell John P.. Combined flywheel energy storage and attitude control apparatus for spacecraft. USP2000096113033.
  11. McMickell, Brett; Fletcher, Mitch. Configurable space station momentum. USP2016129511882.
  12. Bailey David A. ; Heiberg Christopher J. ; Wie Bong. Continuous attitude control that avoids CMG array singularities. USP2000106131056.
  13. Damilano Patrice,FRX. Control of the attitude of a satellite in low orbit involving solar acquisition. USP1998085788188.
  14. Chan Fred N. (Atherton CA) Nilsen Frank C. (Mountain View CA). Digital PWPF three axis spacecraft attitude control. USP1986074599697.
  15. Rodden John J. ; Furumoto Nobuo ; Fichter Walter,DEX ; Bruederle Ernst,DEX. Dynamic bias for orbital yaw steering. USP1998085791598.
  16. Goodzeit,Neil Evan; Lempke,James Donald. Efficient orbit sparing system for space vehicle constellations. USP2006057051980.
  17. Lehner John A. (Sunnyvale CA) Lebsock Kenneth L. (Manhattan Beach CA). Electronic on-orbit roll/yaw satellite control. USP1985064521855.
  18. Savoca Robert C. (Ridgefield CT). Fan scan horizon sensor for a spin stabilized satellite. USP1989054827422.
  19. Goodzeit, Neil Evan. Fault tolerant attitude control system for zero momentum spacecraft. USP2004036702234.
  20. Gschel Wilhelm (Taufkirchen DEX). Method and apparatus for controlling a satellite. USP1981094288051.
  21. Didinsky Garry ; Wu Yeong-Wei Andy. Method and apparatus for estimating attitude sensor bias in a satellite. USP2000086108593.
  22. Peck,Mason A.. Method and system for steering a momentum control system. USP2007037185855.
  23. Schwarzschild Marc (East Brunswick NJ). Method for acquiring three-axis earth pointing attitude for an initially spinning spacecraft. USP1991065020744.
  24. Tessandori, Stephane. Method for characterizing a transmitting antenna of a satellite in orbit and associated system. USP2015069065529.
  25. Smay John W. (Torrance CA) Hummel ; Jr. William F. (Los Angeles CA) Chen Carl L. (Rolling Hills Estate CA) Slafer Loren I. (Los Angeles CA). Method for controlling the spin axis attitude of a spinning spacecraft. USP1989064837699.
  26. Billing-Ross, James A.; Pledger, Douglas B.. Method for determining 3-axis spacecraft attitude. USP1994065319969.
  27. Matthews, Nicholas. Method of and apparatus for returning an earth orbiting spacecraft to an earth pointing attitude after displacement therefrom. USP1991075035381.
  28. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  29. Lange Benjamin O. (Sunnyvale CA) Scheit Arnold (Munich DEX). Method of sun and earth acquisition for three axis stabilized satellites equipped with acquisition sensors. USP1982114358076.
  30. Lawrence P. Davis ; Tristam T. Hyde. Moment control unit for spacecraft attitude control. USP2002016340137.
  31. Peck, Mason Alan; Hyde, Tristram Tupper. Momentum control system and method. USP2004076758444.
  32. Peck,Mason A.. Momentum stabilized launch vehicle upper stage. USP2006087090171.
  33. Tilley Scott W. ; Holmes Thomas J. ; Reckdahl Keith J.. Onboard attitude control using reaction wheels. USP2001096285928.
  34. Hubert Carl H. (East Windsor NJ). Orientation of momentum stabilized vehicles. USP1981064275861.
  35. Bailey David A.. Orienting a satellite with controlled momentum gyros. USP2000116154691.
  36. Stetson ; Jr. John B. (Newtown PA). Reaction wheel fricton compensation using dither. USP1991065020745.
  37. Williams, Paul; Franklin, Steve; Cazeau, Pat; Wang, Grant; Wang, Wendy. Safing mode for high momentum states in body stabilized spacecraft. USP2003046550721.
  38. Cope Paul E. G. (Fareham GB2). Satellite attitude control. USP1988114786018.
  39. Raymond Charles D'Ambrosio ; Minh Ngoc Tran. Satellite attitude control system. USP2002106471161.
  40. Fowell Richard A. (Culver City CA) Yocum John F. (Rancho Palos Verdes CA). Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device. USP1997095667171.
  41. Richard A. Fowell. Satellite spin reorientation using a single degree of freedom momentum storage device. USP2002056382565.
  42. Brderle Ernst (Ottobrunn DEX) Reindler Albrecht (Riemerling DEX). Satellites and roll/yaw controls therefor. USP1985034504912.
  43. Roberts Randy D. (Phoenix AZ) Carter Rodney A. (Phoenix AZ) Ogden Gary J. (Glendale AZ). Single gimbal control moment gyroscope skewed array mounting arrangement. USP1989054825716.
  44. Noyola Richard A. ; Ih Che-Hang C.. Slew rate direction determination for acquisition maneuvers using reaction wheels. USP2000106138953.
  45. Harvey Thomas J. (Los Altos Hills CA) Gibson Gary C. (Los Gatos CA). Space satellite with agile payload orientation system. USP1983034375878.
  46. Reckdahl, Keith; Price, Xenophon. Spacecraft having a momentum wheel configuration that prevents zero wheel speeds. USP2004026691955.
  47. Surauer Michael,DEX ; Roche Christian,DEX ; Fichter Walter,DEX. Sun search method and apparatus for a satellite stabilized in three axes. USP1999055906338.
  48. Goodzeit, Neil Evan; Li, Xipu. Sun sensor alignment compensation system. USP2003106629672.
  49. Shaltiel, Rabin; Kahane, Allan. System and method for measurement of angular orientation of aerospace platforms. USP2015059027888.
  50. Goodzeit, Neil E.. System for geosynchronous spacecraft rapid earth reacquisition. USP2004026695263.
  51. Goodzeit, Neil E.; Weigl, Harald J.. System for on-orbit correction of spacecraft payload pointing errors. USP2004056732977.
  52. Garg Subhash C. (San Jose CA) Gretz Bruce D. (Philadelphia PA). Transition control system for spacecraft attitude control. USP1990064931942.
  53. Reckdahl Keith J.. Wheel speed control system for spacecraft with rejection of null space wheel momentum. USP2000106141606.
  54. Rodden John J. ; Price Xenophon H.. Yaw steering momentum system. USP2001116311932.

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