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특허 상세정보

Aircraft, missile, projectile or underwater vehicle with improved control system and method of using

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/12    B64C-005/10   
미국특허분류(USC) 244/003.26; 244/046
출원번호 US-0292533 (2005-12-02)
등록번호 US-8809755 (2014-08-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian M.
인용정보 피인용 횟수 : 4  인용 특허 : 13
초록

The present invention relates to an aircraft, missile, projectile or underwater vehicle with an improved control system, an improved control system and a method of maneuvering an aircraft, missile, projectile or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, projectile or underwater vehicle with control surfaces that are movable along a track. The present invention further relates to a method of controlling a aircraft, missile, projectile or underwater vehicle using such a control system. One of the technica...

대표
청구항

1. A method comprising: maneuvering an aircraft, missile, projectile or underwater vehicle bysensing a condition which requires a change in the center of pressure or a change in the static or dynamic stability of the aircraft, missile, projectile or underwater vehicle with at least one sensor having an output; andmoving a control surface along a track positioned on the aircraft, missile, projectile or underwater vehicle's bodywherein the moving of the control surface is performed by a control system based in part on the output of the at least one sensor....

이 특허에 인용된 특허 (13)

  1. Shaheen, Milad A.; Dreher, Robert V.. Actuator for aircraft stabilizers with a failure responsive lock control mechanism. USP2004016672540.
  2. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2004026685143.
  3. Shimovetz Ralph. Configurable aerial vehicle aerosurface. USP2001096286789.
  4. Coronel Paul K. (P.O. Box 134 Kailua-Kona HI 96730). Convertible delta wing aircraft. USP1982124365774.
  5. Fanucci,Jerome P.; King,Michael J.; Maass,David P.; Bystricky,Pavel. Extendable joined wing system for a fluid-born body. USP2006016986481.
  6. Shmoldas John D. (Thousand Oaks CA) Hutchings Michael B. (Westlake Village CA) Barlow Christopher W. (Newbury Park CA). Extendable wing for guided missles and munitions. USP1997045615846.
  7. Gough ; Jr. William Albert Gordon (Aldergrove CAX). Method and apparatus for adaptive control. USP1997115687077.
  8. Bryant William F. (Bellevue WA) Nadkarni Arun A. (Kirkland WA) Salo Paul (Seattle WA). Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to at. USP1997095669582.
  9. Ben-Ari, Tsafrir. Method for operating an air-to-air missile and corresponding missile with autonomous or semi-autonomous modes. USP2004096789763.
  10. Coleman Henry L. (1749 Wesley Ave. El Cerrito CA 94530). Method to construct variable area, membrane spar and wing airfoil aircraft and kite wings and suitable aelerons. USP1991105052641.
  11. De Luca Nicholas J. (721 E. Cordova St. #1 Pasadena CA 91101). Recreational and sport rocket construction. USP1993125271579.
  12. Rabinow Jacob (Washington DC) Boyd William Hunter A. (Kensington MD). Rocket. USP1977054024998.
  13. Kaniut Herbert (Orrerweg 33/35 5000 Cologne 71 DT). Shifting horizontal tail with helical motions. USP1977054025007.