摘要
On the base of theoretic analysis of gliding extended range, a mathematic model for exterior ballistics of gliding extended range guided munitions (ERGM) was established, and the maximum lift-to-drag ratio trajectory was simulated to obtain the ideal trajectory and actual trajectory. The simulation results were analyzed, and the improvement measures for the controlling system and the canard rudder surface shape were put forward to solve the oscillation problems of attack and attitude angles, thus assure the ERGM's stabilization of gliding flight.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 13-16 |
| 页数 | 4 |
| 期刊 | Binggong Xuebao/Acta Armamentarii |
| 卷 | 31 |
| 期 | SUPPL. 2 |
| 出版状态 | 已出版 - 12月 2010 |