| 一种新的导弹块对角控制器设计法 |
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| 引用本文： | 胡云安,吴光彬,周绍磊.一种新的导弹块对角控制器设计法[J].航天控制,1999(4). |
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| 作者姓名： | 胡云安 吴光彬 周绍磊 |
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| 作者单位： | 海军航空工程学院!烟台264000 |
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| 摘 要： | 利用小脑关节模型控制器(CMAC) 神经网络辨识了导弹控制系统的几个重要空气动力参数, 证明了估计误差、权误差有界, 然后用解析逆解设计方法、变结构控制方法设计了块对角控制器。仿真结果显示了本文算法的有效性
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| 关 键 词： | 人工神经元网络 非线性系统 数学模型 变结构控制 |
A New Method to Design Block Diagonal Controller of Missile |
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| Hu Yunan Wu Guangbin Zhou Shaolei Naval Aeronautical Engineering Academy,Yantai.A New Method to Design Block Diagonal Controller of Missile[J].Aerospace Control,1999(4). |
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| Authors: | Hu Yunan Wu Guangbin Zhou Shaolei Naval Aeronautical Engineering Academy Yantai |
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| Institution: | Hu Yunan Wu Guangbin Zhou Shaolei Naval Aeronautical Engineering Academy,Yantai 264000 |
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| Abstract: | A few important aerodynamic parameters are identified by using (CMAC) neural network, proved the boundedness of the estimated error and the weight error and then designed the block diagonal controller (BDC) of the missile by means of analytical inverse solution and variable structure control. The simulation results demonstrated the effectiveness of the proposed method. |
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| Keywords: | Artificial neural network Nonlinear system Mathematical model |
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