Abstract
Using ADAMS software, dynamic simulation was done to the two-stage missile with sleeve joint. The aerodynamic forces on the missile in the course of separation were described accurately in ADAMS software. The forces between two stages were calculated. The separation was proved to be rapid and successful. The results were compared with the data which was got through the ballistic simulation, and the two results are similar. So the dynamic simulation means using ADAMS software is correct.
| Original language | English |
|---|---|
| Pages (from-to) | 3512-3514+3519 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 18 |
| Issue number | 12 |
| Publication status | Published - Dec 2006 |
Keywords
- ADAMS
- Aerodynamic force
- Dynamic simulation
- Two-stage separation