Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 610-615 |
| Number of pages | 6 |
| Journal | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
| Volume | 17 |
| Issue number | 5 |
| Publication status | Published - 1997 |
Keywords
- Active control
- Beam
- Launcher
- Vibration analysis
- Vibration control