发明名称 Roll compensated seeker head
摘要 A digital, open-loop control system which compensates for the effects of roll on a missile-carried seeker head such as a radar antenna or an infrared sensor. The system utilizes a roll rate gyro affixed to the missile body for sensing the missile roll rate, developing a digital signal in proportion to the sensed roll rate, and using the digital signal in open-loop fashion to actuate a stepping servomotor for repositioning the seeker head so as to stabilize the same relative to the target irrespective of missile roll movements.
申请公布号 US4266173(A) 申请公布日期 1981.05.05
申请号 US19790020577 申请日期 1979.03.15
申请人 THE BOEING COMPANY 发明人 MCTIGUE, LARRY D.;PINSON, GEORGE T.
分类号 F41G7/22;(IPC1-7):B64C13/18 主分类号 F41G7/22
代理机构 代理人
主权项
地址