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특허 상세정보

Terminal guidance method and a guided missile operating according to this method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/22    F42B-025/24   
미국특허분류(USC) 244/322 ; 102/384 ; 244/316
출원번호 US-0446728 (1982-12-03)
우선권정보 FR-0023025 (1981-12-09)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 8
초록

A guidance method is provided for the terminal portion of the trajectory of a guided missile having a sensor and comprising two sections coupled together by a central shaft and free to rotate with respect to one another about the longitudinal axis of the missile; one section comprises a drive means for controlling the roll attitude of this section and a gas generator which feeds a nozzle for providing a transverse throat force and the other section has a stabilizing tail unit formed by a set of fins able to be opened out.

대표
청구항

A method for guiding a missile during a terminal portion of the missile\s trajectory, said missile having a sensor with a beam said sensor being sensitive to energy radiated by a potential target comprising the following steps for seeking the target: (a) immobilizing the beam of the sensor along the longitudinal axis of the missile; (b) imparting to the missile: a rotation about the longitudinal axis of the missile at a given angular roll speed, and a spiral line movement in order that the beam of the sensor describes a surface of revolution by creating ...

이 특허를 인용한 특허 피인용횟수: 21

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Utreja Laipat R. (Harvest AL) Gurley William H. (Huntsville AL). Aircraft hollow nose cone. USP1989074850275.
  3. Stessen Lothar (Lauf/Pegnitz DEX). Ammunition article controllable during its final flight phase and method for navigation thereof towards a target. USP1987064674408.
  4. Argyrakis Nikolaus (Nuremberg DEX). Ammunition incorporating searching fuse with trajectory correctable during its final flight phase and method for combati. USP1987124711178.
  5. Kirshman, David J.; Deamer, David A.. Cavity flow shock oscillation damping mechanism. USP2013058436284.
  6. Goltz, Gerhard; Grosswendt, Werner; Peller, Helmut; Seidensticker, Jens. Fin stabilized subammunition body. USP1991085037040.
  7. Harraeus Egbert,DEX ; Obkircher Bernt,DEX. Method and apparatus for combatting helicopters operating with concealment. USP1999025874727.
  8. Sundermeyer Peter (Lauf/Pegn DEX). Method and utilization of final flight phase-corrected submunition for the attacking of armored shelters cross-reference. USP1989054831935.
  9. Kinsey, Jr., Lloyd E.; Cook, James M.. Method of controlling missile flight using attitude control thrusters. USP2011118058596.
  10. Yanushevsky,Rafael T.. Methods and systems for guiding an object to a target using an improved guidance law. USP2007037185844.
  11. Miralles, Carlos Thomas. Multimode unmanned aerial vehicle. USP20190310222177.
  12. Miralles, Carlos Thomas. Multimode unmanned aerial vehicle. USP2015099127908.
  13. Mayersak Joseph R.. Precision guidance system for aircraft launched bombs. USP2001076254031.
  14. Zacharias Athanassios,DEX. Process for guiding a flying object and flying objects. USP1999035880396.
  15. Romer Rudolf,DEX ; Wollmann Gerd,DEX. Projectile having an apparatus for flight-path correction. USP1998115836540.
  16. Schleimann-Jensen Lars J. (182 34 Danderyd Ekbacksvagen SEX). Projectile steering apparatus and method. USP1990104966078.
  17. Jones, James F.; Kast, Brian A.; Kniskern, Marc W.; Rose, Scott E.; Rohrer, Brandon R.; Woods, James W.; Greene, Ronald W.. Small caliber guided projectile. USP2010087781709.
  18. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  19. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  20. Schleimann-Jensen Lars J. (Ekbacksvgen 33A 182 34 Danderyd SEX). System for guiding a flying object towards a target. USP1990014890554.
  21. Mark H. Yim. Tracking device. USP2002076422509.