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특허 상세정보

Apparatus for controlling the attitude of and stabilizing an elastic body

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/26    B64G-001/28/1/36    B64G-001/38   
미국특허분류(USC) 244/164 ; 244/165 ; 244/169 ; 244/170
출원번호 US-0359760 (1989-07-14)
우선권정보 DE-3731087 (1987-09-16)
국제출원번호 PCT/DE88/00581 (1988-09-16)
§371/§102 date 19890714 (19890714)
국제공개번호 WO-8902622 (1989-03-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 18  인용 특허 : 16

A device is disclosed for regulating a set value and/or for stabilizing elastic objects subject to spin and free to move around their axis of rotation, in particular aircraft and spacecraft. For that purpose, the regulating signals required to regulate the set value or to stabilize the freely moving objects can be obtained by means of a regulator having a transfer function with a denominator degree about three orders higher than the numerator.


Apparatus for controlling the attitude of and stabilizing an elastic body having a bias angular momentum with associated spin axis and being free to rotate about three mutually orthogonal body axes, especially aircraft and space vehicles, with respect to reference values for two of said body axes disposed transversely to said spin axis, said two body axes being vehicles axes, by means of an attitude sensor measuring deviations of a first one of said transverse axes from a reference direction, at least one controller, at least one modulator and at least o...

이 특허에 인용된 특허 (16)

  1. 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.
  2. Izumida Kiichiro (Kanagawa JPX) Kasai Ritaroh (Kanagawa JPX). Artificial satellite attitude control system. USP1986104617634.
  3. Broquet Jean B. (Saint Cyr l\Ecole FRX). Attitude control systems for space vehicles. USP1981104294420.
  4. Bruderle Ernst (Ottobrunn DEX) Gottzein Eveline (Oberpframmern DEX) Bittner Helmut (Munich DEX). Controller for the attitude stabilization of a satellite. USP1979114174819.
  5. Chan Fred N. (Atherton CA) Nilsen Frank C. (Mountain View CA). Digital PWPF three axis spacecraft attitude control. USP1986074599697.
  6. Lehner John A. (Sunnyvale CA) Lebsock Kenneth L. (Manhattan Beach CA). Electronic on-orbit roll/yaw satellite control. USP1985064521855.
  7. Chan Fred N. (Atherton CA). Hysteresis conditioner for spacecraft attitude control. USP1986054591118.
  8. Muhlfelder Ludwig (Livingston NJ) Phillips Kevin J. (Hightstown NJ) Blasnik Steven L. (Cambridge MA). Magnetically torqued nutation damping. USP1984014424948.
  9. Gschel Wilhelm (Taufkirchen DEX). Method and apparatus for controlling a satellite. USP1981094288051.
  10. Chan, Fred N.. Method and apparatus for thruster transient control. USP1985084537375.
  11. Vorlicek Preston L. (Memphis TN). Method for spinning up a three-axis controlled spacecraft. USP1988024725024.
  12. 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.
  13. Phillips Kevin J. (Hightstown NJ). Nutation damping in a dual-spin spacecraft. USP1981064272045.
  14. Brderle Ernst (Ottobrunn DEX) Reindler Albrecht (Riemerling DEX). Satellites and roll/yaw controls therefor. USP1985034504912.
  15. Garg Subhash C. (San Jose CA) Bhat Mahabaleshwar K. P. (San Jose CA). Spacecraft attitude control using coupled thrusters. USP1989074848706.
  16. Hubert Carl H. (East Windsor NJ) Miller Paul A. (Hamilton NJ). Spacecraft stabilization system and method. USP1988074758957.

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  2. Harmse,Magiel J.; Zheng,Qingsheng. Automated closed loop step testing of process units. USP2007047209793.
  3. Challoner A. Dorian ; Rosen Harold A.. Dynamic decoupler for improved attitude control. USP1998105816538.
  4. Patera, Russell Paul. Energy-angular momentum closed-loop guidance for launch vehicles. USP2013108571727.
  5. Patera, Russell Paul. Energy-angular momentum diagnostic method for launch vehicle performance. USP2014038676407.
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  9. John S. Higham ; Rhys Kevin Adsit. Pre-bias scheme for roll momentum unloads on pitch momentum bias/yaw reaction wheel spacecraft. USP2002086439509.
  10. Surauer Michael (Chieming DEX) Bittner Helmut (Munich DEX). Process and a device for controlling the attitude of a three-axis stabilized spinning spacecraft. USP1997015597143.
  11. 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. USP2010097797085.
  12. Nakamura Taichi,JPX. Rendezvous spacecraft collision avoidance device. USP1999025868358.
  13. Hoffmann, Heiko; Payton, David W.. Self-stabilizing system for multiple interacting controllers. USP2017019557722.
  14. Hinnant, Jr., Harris O.; Brekke, Darin W.; Black, Jr., David J.. Structural health management with active control using integrated elasticity measurement. USP2015129221555.
  15. Calise Anthony J. ; Kim Byoung-Soo,KRX. System and method for adaptive control of uncertain nonlinear processes. USP2000076092919.
  16. Calise,Anthony J.; Kim,Byoung Soo. System and method for adaptive control of uncertain nonlinear processes. USP2007027177710.
  17. Corban,J. Eric. System and method for adaptive control of uncertain nonlinear processes. USP2006057039473.
  18. Potter,Calvin C.; Evans,Paul S.; Keller,Terry L.. Thrust vector actuation control system and method. USP2007037185857.