Missile launching device |
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| 申请号 | JP19836388 | 申请日 | 1988-08-09 | 公开(公告)号 | JPH0250093A | 公开(公告)日 | 1990-02-20 |
| 申请人 | Mitsubishi Electric Corp; | 发明人 | KAMEI NOBUO; | ||||
| 摘要 | PURPOSE:To permit the remarkable reduction of a vibration upon launching by a method wherein a control power for reducing the vibration effectively utilizing the reaction force of a movable mass is applied on a launching tube by an actuator. CONSTITUTION:A movable mass 4 is attached movably to a launching tube 2 through a spring 5 and an actuator 6. An accerometer 7 detects the vibrating speed of the launching tube 2 through the integrator 9 of a controller 8 and generates a control force, proportional to the vibrating speed and having a reversed direction to the vibrating speed, in the actuator 6 through an electric power amplifier 10. The actuator 6 is constituted of a fixed core 11 and a movable core 12. A missile launching device 1 is added with a vibration controlling function in such a manner whereby the launching accuracy of a missile 3 may be improved and the affection of the vibration to a not yet launched missile may be reduced when the launching device 1 is provided with a plurality of launching tubes 2. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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