Abstract
In order to study the dynamic response of the vehicular guided missile launcher during launching aslant, a coupled rigid and flexible model based on FEA software and computational dynamics of multibody systems software was used to simulate the dynamic process. The factors which influenced to the dynamic process, such as jet flow, hydraulic equipment distortion, bodywork distortion, revolver distortion and bracket distortion, etc. were considered and analyzed quantitatively. The study has demonstrated that the coupled rigid and flexible model has a great capability for simulating missile launch processes and studying the disturbances.
| Original language | English |
|---|---|
| Pages (from-to) | 1789-1791+1796 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 21 |
| Issue number | 6 |
| Publication status | Published - 20 Mar 2009 |
Keywords
- Coupled rigid and flexible model
- Influence coefficient
- Launching dynamics
- Structure distortion