| 静不稳定制导火箭弹控制系统设计 |
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| 引用本文： | 杨明,毛昱天,李浩,张锐.静不稳定制导火箭弹控制系统设计[J].导航定位于授时,2017,4(2):35-40. |
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| 作者姓名： | 杨明 毛昱天 李浩 张锐 |
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| 作者单位： | 中国兵器工业导航与控制技术研究所,北京,100089 |
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| 基金项目： | “十三五”陆军预先研究课题 |
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| 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。
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| 关 键 词： | 静不稳定 制导火箭弹 自动驾驶仪 |
Design of Autopilot for Guided Rocket
with Relaxed Static Stability |
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| YANG Ming,MAO Yu-tian,LI Hao and ZHANG Rui.Design of Autopilot for Guided Rocket
with Relaxed Static Stability[J].Navigation Positioning & Timing,2017,4(2):35-40. |
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| Authors: | YANG Ming MAO Yu-tian LI Hao and ZHANG Rui |
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| Institution: | Chinese Ordnance Navigation and Control Technology Research Institute,Chinese Ordnance Navigation and Control Technology Research Institute,Chinese Ordnance Navigation and Control Technology Research Institute and Chinese Ordnance Navigation and Control Technology Research Institute |
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| 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 |
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| Keywords: | Static instability Guided rocket Autopilot |
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