|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/003.15 ; 244/003.1 ; 244/003.24|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 32 인용 특허 : 7|
A system for intercepting targets having predictable flight trajectory, the system comprising a platform carrying an interceptor missile which includes a seeker unit, propulsion system steering system and destruction capability system, all communicating with a processor device. The processor device is further coupled to a data link for communicating with the platform. In response to launching of the intercepting missile, the processor device controls the steering system and propulsion system for steering the missile in one of the following flight modes: ...
[What is claimed is:] [1.](i) a platform carrying at least one interceptor missile; the interceptor missile includes a seeker unit, propulsion system, steering system, and target destruction capability system all communicating with a processor device; said processor device is further coupled to a data link for communicating with at least said platform;(ii) the processor device, in response to launching of said interceptor missile, for controlling said steering system and propulsion system for steering said missile in at least the following flight modes:(...