发明名称 Simplified high accuracy guidance system
摘要 A simplified guidance system for air-to-air missiles where the pilot adjusts his helmet sight to compensate for missile errors and this information is fed to a computer which computes correction data from error information, aircraft position information and missile position information, correction data is then sent via a radio link to the missile control system which changes the flight path accordingly.
申请公布号 US4146196(A) 申请公布日期 1979.03.27
申请号 US19760706048 申请日期 1976.07.20
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 SCHULTZ, ROBERT L.
分类号 F41G3/22;F41G7/30;(IPC1-7):F41G3/16;F41G7/10;F41G9/00 主分类号 F41G3/22
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