发明名称 |
Missile steering system using a segmented target detector and steering by roll and pitch maneuvers |
摘要 |
A missile control and guidance system employing a combination of generally vertically disposed ailerons and generally horizontally disposed elevators. In order to make a horizontal turn, a combination of aileron and elevator deflections is used, to cause the missile to make a "blanked" turn. The ailerons and elevators are controlled by servos activated by a logic circuit. The logic circuit is connected to a segmented target detector. The missile will maneuver depending on which of the segments of the detector "sees" a target.
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申请公布号 |
US4381090(A) |
申请公布日期 |
1983.04.26 |
申请号 |
US19670687924 |
申请日期 |
1967.11.27 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
GARNER, WILLIAM G. |
分类号 |
F41G7/22;(IPC1-7):F41G7/22;F42B15/02 |
主分类号 |
F41G7/22 |
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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