摘要
From the simplified model of rocket and/or missile launcher, the beam vibration excited by the moving rigid body was analyzed. The optimal inputs were given on the basis of the optimal control theory. The simulation test showed that the input suppressed the vibration of the beam and the initial disturbance of the rocket.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 610-615 |
| 页数 | 6 |
| 期刊 | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
| 卷 | 17 |
| 期 | 5 |
| 出版状态 | 已出版 - 1997 |