发明名称 |
Trajectory shaping of anti-armor missiles via tri-mode guidance |
摘要 |
In a missile system, a simple way to guide a missile in a predetermined trajectory from launch to the impacting with a target for optimum warhead penetration of armor by a guided missile. Initially, the missile is guided in yaw by proportional navigation. Subsequently it is guided in pitch first by a pitch programmer until the missile reaches a predetermined gimbal angle between a line of sight of a seeker of the missile and a centerline of the missile, then in pitch by a pseudo-time-optimal closed loop controller to direct the missile pitch attitude at a predetermined rate toward a target until said missile reaches another predetermined gimbal angle, and finally by proportional navigation in pitch of the missile to the target.
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申请公布号 |
US4277038(A) |
申请公布日期 |
1981.07.07 |
申请号 |
US19790034088 |
申请日期 |
1979.04.27 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY |
发明人 |
YATES, ROBERT E.;LEONARD, JOHN P.;ALONGI, ROBERT E.;ALBANES, WILFREDO V.;BISHOP, CHARLES M. |
分类号 |
F41G7/00;F41G7/22;F41G7/34;(IPC1-7):F42B15/02 |
主分类号 |
F41G7/00 |
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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