| 摘要: |
| 选取鸭式布局结构制导火箭弹作为研究对象,从改善制导火箭弹的飞行性能的要求出发,对静不稳定火箭弹自动驾驶仪进行了设计,对弹道上不同飞行高度和不同飞行速度条件下的自动驾驶仪响应进行仿真研究,结果表明,所设计的自动驾驶仪能够保证控制系统的性能稳定。 |
| 关键词: 静不稳定 制导火箭弹 自动驾驶仪 |
| DOI： |
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| 基金项目: |
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| Design of Autopilot for Guided Rocket with Relaxed Static Stability |
| YANG Ming,MAO Yu-tian,LI Hao,ZHANG Rui |
| (Chinese Ordnance Navigation and Control Technology Research Institute) |
| Abstract: |
| The autopilot is designed for relaxed static stable guided rocket with canard configuration to improve the flight performance, nontrivial numerical simulations are performed to verify the effectiveness of the devised autopilot for different altitudes and velocities on the trajectory, the results of which demonstrate that the stability of the control system could be guaranteed |
| Key words: Static instability Guided rocket Autopilot |
