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.
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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 |
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代理人 |
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主权项 |
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地址 |
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