发明名称 Scanning beam beamrider missile guidance system
摘要 A beamrider guidance system for missiles wherein a laser beam is given two circular motions around the boresight axis to produce amplitude and phase modulation on the signal received at the missile. The information on distance from boresight is contained in the amplitude modulation and the angular information is contained as phase modulation. A laser optical system with a spinning holographic element provides one of the circular motions for the beam. The other circular motion is provided by a low frequency, circular scanning mirror.
申请公布号 US4516743(A) 申请公布日期 1985.05.14
申请号 US19830486127 申请日期 1983.04.18
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 SWEENEY, DONALD W.;GALLAGHER, NEAL C.;CHRISTENSEN, CHARLES R.
分类号 F41G7/26;(IPC1-7):F41G7/26 主分类号 F41G7/26
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