| 发明名称 |
Missile maneuver concept |
| 摘要 |
A lifting body missile is controlled by pitch and roll commands wherein the yaw autopilot is caused to change in accordance with the roll and estimated angle of attack input information. A command logic is provided to determine the polarity of the command signals to the autopilot.
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| 申请公布号 |
US4044237(A) |
申请公布日期 |
1977.08.23 |
| 申请号 |
US19760667819 |
申请日期 |
1976.03.16 |
| 申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
COWGILL, PAUL N.;PEARSON, JOHN L. |
| 分类号 |
F41G7/30;G05D1/10;(IPC1-7):G06F15/50;F42B15/02 |
主分类号 |
F41G7/30 |
| 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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