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.
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
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