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.
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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 |
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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