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특허 상세정보

Active nutation control system for space vehicle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/10    G05D-001/08   
미국특허분류(USC) 364/434 ; 244/322 ; 244/169 ; 364/459
출원번호 US-0114197 (1980-01-22)
우선권정보 FR-0001663 (1979-01-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 5
초록

An active nutation control system for a space vehicle spinning about a geometric axis has thrusters for creating an external torque about an axis transverse to the first. The amplitude of the nutation and its phase in relation with the spinning movement are detected. A control arrangement receives signals from the nutation detectors, computes the changes in the angular direction of the angular momentum of the vehicle caused by thruster activation and energizes the thrusters when contemporaneously the amplitude of the nutation movement is greater than a p...

대표
청구항

An active nutation control system for a space vehicle spinning about one of its geometrical axes, having: means for creating pulses of external rocking torque about an axis transverse to said geometrical axis; means carried by said space vehicle for delivering a periodically varying signal having an amplitude representative of the magnitude of the nutation of said space vehicle and a frequency equal to the nutation frequency of said space vehicle; and control means for controlling the torque-creating means, comprising: first enabling means to deliver a s...

이 특허를 인용한 특허 피인용횟수: 14

  1. Raman Kidambi V. (East Windsor NJ) Muhlfelder Ludwig (Livingston NJ) Hubert Carl H. (Cranbury NJ) Furia Thomas J. (Ambler PA). Attitude control system. USP1990044916622.
  2. Phillips Kevin J. (East Windsor NJ) Tracy Terry G. (Cranbury NJ). Control of nutation in a spacecraft. USP1985034504032.
  3. Challoner A. Dorian ; Rosen Harold A.. Dynamic decoupler for improved attitude control. USP1998105816538.
  4. Yehezkeli,Oded; Kunreich,Irad. Method and system for adjusting the flight path of an unguided projectile, with compensation for jittering deviation. USP2008127467761.
  5. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  6. Gnemmi,Patrick; Charon,Romain; Samirant,Michel. Projectile steering by plasma discharge. USP2006027002126.
  7. Cope Paul E. G. (Fareham GB2). Satellite attitude control. USP1988114786018.
  8. Fowell Richard A. ; Tanner Thomas M.. Satellite spin vector control with sun sensor. USP1999035884869.
  9. Scott Peter R. (Stevenage GB2). Spacecraft nutation damping. USP1986054591117.
  10. Crawford, James I.; Howell, W. Max. Spin stabilized impulsively controlled missile (SSICM). USP1985124560120.
  11. Zemany Paul D. (Amherst NH) Smith Kirby A. (Derry NH) Smith John A. (Bedford MA). State-deviation-estimation circuit employing a phase-locked-loop phase reference. USP1988124791573.
  12. Grosso Vincent A. (Hopkinton MA) Fitzgerald Robert J. (Wayland MA) DeFonzo Richard J. (Northboro MA). Strap down roll reference. USP1987064676456.
  13. Liu, Dan Y.; Wang, Qinghong W.; Chiang, Richard Y.. Systems and method of controlling a spacecraft using attitude sensors. USP2013128620496.
  14. Garg Subhash C. (San Jose CA) Gretz Bruce D. (Philadelphia PA). Transition control system for spacecraft attitude control. USP1990064931942.