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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0274683 (1972-07-24) |
발명자 / 주소 |
|
인용정보 | 피인용 횟수 : 7 인용 특허 : 0 |
A guidance system for a missile or other vehicle utilizing a gyro stabilized seeker which is arranged in such a manner with respect to the missile as not to be servo controlled, but rather to follow the missile air-frame by means of passive coupling between seeker and airframe, as the airframe is st
An inertially stabilized seeker comprising a housing, a stabilized seeker element operatively disposed in said housing, and passive coupling means in said seeker functioning to cause said seeker element to move to orient itself with said housing, such movements taking place at a rate proportional to
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