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超机动飞行的神经网络动态逆控制 被引量:2

Neural Network Dynamic Inversion Control and Simulation of Supermaneuverable Flight
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摘要 根据反馈线性化理论 ,讨论了神经网络自适应非线性动态逆控制设计。首先根据时标分离的原则 ,采用动态逆方法设计了快回路和慢回路控制器 ;其次提出了基于模型逆的神经网络非线性直接自适应控制方案 ,其中设计一种在线神经网络用于补偿模型逆误差。仿真表明 ,该控制方案具有较好的自适应能力和鲁棒性。 A discussion is devoted to the design of a self adaptive and nonlinear dynamic neural network inversion controller according to the feedback linearization theory. The control of uncertain nonlinear systems is an active subject in the modern control area, and there are a lot of research results about them. Neural networks(NN) are widely used to control nonlinear systems, so a lot of control methods have been proposed. But most of them are control methods of single input and single output nonlinear systems. There are few control methods of multi input and multi output uncertain nonlinear systems. The discussion in this paper is focused on multi input and multi output uncertain nonlinear systems. Firstly, with two time scale, the design of a fast loop controller and a slow loop one is given by using the dynamic inversion method. Secondly, a neural network nonlinear, direct and self adaptive scheme based is presented a model inversion, in which an online neural network is designed to compensate the model inversion errors. It is demonstrated by the distributed simulation of a local area network that this adaptive control design has good adaptability and robustness.
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2003年第2期168-172,共5页 Journal of Nanjing University of Aeronautics & Astronautics
基金 国家自然科学基金 (60 1 740 45 ) 航空第一集团基金 (0 1 D5 2 0 2 5 )资助项目
关键词 超机动飞行 神经网络 动态逆控制 自适应控制 飞机 model inversion neural network adaptive control
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参考文献5

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二级参考文献2

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