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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F41G-007/14 F41G-009/00 F41G-007/00 F41G-011/00|
|미국특허분류(USC)||244/319 ; 244/314|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 14 인용 특허 : 0|
A system for enabling homing by a missile onto a target which is marked by a beacon at some other location. A radio frequency beacon is located remotely from the intended target. Target coordinates relative to the beacon are obtained and relayed by conventional means to the launch site and are stored in missile memory. During flight the missile seeker acquires, interrogates and tracks the beacon. The missile borne equipment generates guidance signals which alter the trajectory to the target location.
A system for enabling homing of a missile onto a target, said target having a radio frequency beacon disposed at a remote predetermined distance and direction therefrom: a missile having computer means thereon for storing signals indicative of the distance and direction of said target relative to said beacon for storing signals indicative of the inverse of the coordinates of said target; seeker means carried by said missile for acquiring and tracking beacon radiations, said seeker means disposed for emitting signals indicative of spatial coordinates ther...