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특허 상세정보

System, method and computer program product for providing for a course vector change of a multiple propulsion rocket propelled grenade

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/22    F42B-015/01    F41G-003/14    G05D-001/12    G05D-001/08    F41G-007/20    F41G-007/00    F42B-015/00   
출원번호 US-0631108 (2015-02-25)
등록번호 US-9366514 (2016-06-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sanks, Esq., Terry M.
인용정보 피인용 횟수 : 1  인용 특허 : 25
초록

Embodiments relate to a projectile system, method and computer program product for controlling the flight of a projectile to make a course change by approximately 90°, greater than 90° or up to 90°. The projectile system comprises a gun-fired projectile having a body, at least one tail fin, a motor firing during a first flight phase and during a second flight phase and at least one controllable canard. The projectile system includes one or more processors configured to determine a turn maneuver profile to a target during the first flight phase, produce c...

대표
청구항

1. A projectile system comprising: a gun-fired projectile having a body including an aft section and a forward section, at least one tail fin coupled to the body at the aft section, a motor configured to fire during a first flight phase and fire during a second flight phase and at least one controllable canard located on the body; andone or more processors configured to determine a turn maneuver profile to a target during the first flight phase, produce control signals to destabilize the body, create a pitch attitude change for the turn maneuver profile ...

이 특허에 인용된 특허 (25)

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  17. Martinez, Marcelo Edgardo. Rolling projectile with extending and retracting canards. USP2012118319164.
  18. McCowan Wayne L. ; Wright Alfred M. ; Garrison Cheryl S. ; Mitchell Robert R.. Scatterider guidance system for a flying object based on maintenance of minimum distance between the designating laser beam and the longitudinal axis of the flying object. USP2000106138944.
  19. Crabtree, Daniel. Ship self-defense missile weapon system. USP2003086610971.
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  21. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Elkton MD) Nevrincean Andrew G. (Elkton MD) Carr ; Jr. Clyde E. (Lincoln University PA). Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture. USP1997025600946.
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