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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

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
초록

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, ...

대표
청구항

[ 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.
  2. Nobel Charles I. (Newtown Square PA). Adaptive autopilot. USP1991105058836.
  3. von Pragenau George L. (Huntsville AL) Rupp Charles C. (Huntsville AL). Attitude control system. USP1976103984072.
  4. Howell ; Thomas H.. Automatic balancing concept. USP1978094116404.
  5. Cannon James J. (Northridge CA) Elkanick Mark (Tucson AZ). Blended missile autopilot. USP1997015590850.
  6. Depew ; Jr. Herbert D. (Los Altos CA) Ernst ; Jr. Robert J. (Los Altos CA). Control system. USP1995085439188.
  7. Dunn Albert J. (Bangor ; Co. Down GB5). Control systems for moving bodies. USP1995025393012.
  8. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  9. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP1998115835869.
  10. Alford Robert L. (Excelsior MN) Rupert John G. (Mahtomedi MN). Electro-mechanical roll control apparatus and method. USP1995095452864.
  11. Forsmo Dennes P. (Acton MA). Fin command mixing method. USP1992025088658.
  12. Pritchard Alan J. (British Aerospace PLC ; Dynamics Group ; Six Hills Way Stevenage ; Hertfordshire ; SG1 2AS GB2) Stanley John D. (British Aerospace PLC ; Dynamics Group ; Six Hills Way Stevenage ; . Guidance systems. USP1989054830311.
  13. Lachmann Karl-Heinz (Lauf-Pegn. DEX) Sundermeyer Peter (Lauf-Pegn. DEX) Schreier Johann (Ruckersdorf DEX) Reindler Albrecht (Lauf-Schonberg DEX) Leininger Jurgen (Lauf/Pegn. DEX). Guided artillery projectile with trajectory regulator. USP1989114883239.
  14. Bagley Cloy J. (Fountain Valley CA). Lateral thrust assembly for missiles. USP1992075129604.
  15. Holm Anders (Karlskoga SEX) Axinger Jan (Storfors SEX) Jarnryd Kenneth (Hagersten SEX). Method and apparatus for imparting to an airborne warhead a desired pattern of movement. USP1997105679919.
  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.
  18. Pinson George T. (Huntsville AL). On-board flight control drag actuator system. USP1986114624424.
  19. Pinson George T. (Huntsville AL). On-board flight control panel system. USP1987104699333.
  20. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  21. Faupell Lawrence C. (Logan UT) Wassom Steven R. (Smithfield UT). Reduced fin span thrust vector controlled pulsed tactical missile. USP1989094867393.
  22. Waymeyer Walter K. (LaVerne CA) Banach Timothy P. (Chino CA). Roll damper for thrust vector controlled missile. USP1993115259569.
  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.
  25. Raynaud Jacques (Savigny-sur-Orge FRX) Darmois Jean (Bourg-la-Reine FRX) Jolivet Pierre (Arcueil FRX) Guillot Jean (Chatenay-Malabry FRX). System for piloting a missile by means of lateral gaseous jets and missile comprising such a system. USP1985074531693.
  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.
  28. Kranz Walter (Taufkirchen DEX). Thrust nozzle system. USP1986054589594.
  29. Fidler John E. (Los Gatos CA). Venting apparatus for controlling missile underwater trajectory. USP1991125070761.
  30. Wiemer Peter (Meerbusch DEX) Grosswendt Werner (Ratingen DEX). Yaw angle free projectile. USP1996105564651.