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특허 상세정보

Method and apparatus for rapidly turning a vehicle in a fluid medium

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/003.22 ; 244/003.1 ; 244/003.15 ; 244/003.21
출원번호 US-0183502 (1998-10-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sidley Austin Brown & WoodSadacca
인용정보 피인용 횟수 : 6  인용 특허 : 30

In a first aspect, the invention uses the thrust and axial aerodynamic forces of and on the missile system as the primary mechanism for altering the missile system's flight path as opposed to the missile system's aerodynamic normal force. In accordance with this first aspect, a first embodiment is a method for changing the direction of travel of a vehicle moving through a fluid medium to a desired direction of travel measured in the vehicle's inertial frame of reference, the vehicle comprising a body including a nose, a moment generating control device, ...


[ What is claimed:] [81.]81. A vehicle adapted for rapid redirection of the flight path and velocity as the vehicle is moving through a fluid medium at a velocity adequate for producing flight sustaining aerodynamic forces on the vehicle, said vehicle comprising:a body including a nose;a plurality of control devices, said control devices being-adapted to impart either a moment or a force to the vehicle in a manner such that the flight path and the velocity of the vehicle are rapidly redirected, said plurality of control devices comprising at least:a forw...

이 특허에 인용된 특허 (30)

  1. Williams Andrew S. (Brea CA). Actuator system and method. USP1997015593109.
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  10. Alford Robert L. (Excelsior MN) Rupert John G. (Mahtomedi MN). Electro-mechanical roll control apparatus and method. USP1995095452864.
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  16. Shafer Daniel E. (Bellevue WA). Missile control system using virtual autopilot. USP1992035094406.
  17. Hatalsky William M. ; Facciano Andrew B. ; Haight Stephen D. ; Johnson Sean A. ; Jordan Aszetta D.. Missile jet vane control system and method. USP1998095806791.
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  20. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
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  23. Tilley Scott W. (Belmont CA) Liu Tung Y. (Union City CA) Higham John S. (Mountain View CA). Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters. USP1994095349532.
  24. Osder Stephen S. (Scottsdale AZ). Stability augmentation system for relaxed static stability aircraft. USP1979104171115.
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  26. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  27. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral nozzles. USP1991125074492.
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