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특허 상세정보

Inertial boost thrust vector control interceptor guidance

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/30    F42B-015/01    F41G-007/00    F42B-015/00   
미국특허분류(USC) 244/003.11; 244/003.1; 244/003.14; 089/001.11; 342/061; 342/062; 342/175; 342/195
출원번호 US-0935687 (2007-11-06)
등록번호 US-8288696 (2012-10-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Howard IP Law Group, PC
인용정보 피인용 횟수 : 5  인용 특허 : 44
초록

A method for engaging a target missile includes sensing the position of the target and of an interceptor missile, and determining time-to-go to intercept and direction of thrust of the interceptor. A one-step intercept solution is determined based on position estimates of the target and the interceptor and is used to iteratively estimate at least two components of a three-dimensional unit thrust vector, and apply updated guidance commands to the interceptor. A system for thrust vector control of an interceptor against a target missile includes a processo...

대표
청구항

1. A method for thrust vector control of an interceptor against a target missile, said method comprising the steps of: sensing at least position and velocity of said target missile to thereby generate a stream of sensed target signals;processing said stream of sensed target signals to produce estimates of at least position and velocity of said target missile;launching an interceptor missile toward an estimated intercept position of said target missile;generating signals representing at least position and velocity of said interceptor missile;determining a...

이 특허에 인용된 특허 (44)

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