| 基于专家PID的滚转导弹控制系统 |
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| 引用本文： | 陈圣,王旭刚,郭新民. 基于专家PID的滚转导弹控制系统[J]. 兵工自动化, 2014, 0(1): 89-90,96 |
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| 作者姓名： | 陈圣 王旭刚 郭新民 |
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| 作者单位： | [1]南京理工大学能源与动力工程学院,南京210094 [2]山西淮海工业集团,山西长治046012 |
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| 摘 要： | 针对滚转导弹俯仰和偏航通道较强的气动不确定性和运动耦合,设计了一种专家PID控制系统。建立了滚转导弹的动力学模型,并采用十字舵来控制俯仰和偏航通道,利用专家PID控制方法设计该导弹的控制系统,并在Matlab中对控制系统进行仿真。仿真结果表明:该控制器能满足良好的性能要求,具有较强的鲁棒性和自适应性,能有效应对俯仰和偏航通道产生较强气动和运动耦合。
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| 关 键 词： | PID 专家PID 滚转导弹 过载控制 |
Control System Design for Rolling Missile Based on the Expert PID |
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| Chen Sheng,Wang Xugang,Guo Xinmin. Control System Design for Rolling Missile Based on the Expert PID[J]. Ordnance Industry Automation, 2014, 0(1): 89-90,96 |
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| Authors: | Chen Sheng Wang Xugang Guo Xinmin |
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| Affiliation: | 1. School of Energy ＆ Power Engineering, Nanjing University of Science ＆ Technology, Nanjing 210094, China; 2. Shanxi Huaihai Industry Group Company, Changzhi 046012, China) |
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| Abstract: | Due to the rolling missile pitch and yaw channels generate strong aerodynamic uncertainty and kinematic coupling, the control system of expert PID is designed. At first, build the dynamic model of rolling missile, at second use cruciform of rudders to control the pitch and yaw channels, then design the control system of rolling missile based on expert PID. At last simulate the control system in a matlab environment. The simulation results show that the controllers can meet performance requirements, it also has better robustness and adaptability which effectively respond to the pitch and yaw channels stron~ aerodvnamic and kinematic couoling. |
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| Keywords: | PID- expert PID roll missile overload control |
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