|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|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 44|
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...
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...