发明名称 |
Quasi-stabilization for line of sight guided missiles |
摘要 |
An open loop reduction in gunner aiming error is provided by a rate gyro feedback to the missile command electronics. The low frequency movements are filtered out of the feedback circuit; permitting tracking of low frequency crossing targets, while eliminating higher frequency gunner jitter inputs.
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申请公布号 |
US4378918(A) |
申请公布日期 |
1983.04.05 |
申请号 |
US19810223863 |
申请日期 |
1981.01.09 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
MILLER, JR., WALTER E.;MCKELVY, JAMES W. |
分类号 |
F41G7/24;F41G7/30;(IPC1-7):F41G7/20 |
主分类号 |
F41G7/24 |
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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