首页> 外文会议>Intelligent Control, 2002. Proceedings of the 2002 IEEE International Symposium on >Adaptive control of limit cycle for unknown nonlinear hysteretic system using dynamic recurrent RBF networks
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Adaptive control of limit cycle for unknown nonlinear hysteretic system using dynamic recurrent RBF networks

机译:基于动态递归RBF网络的未知非线性滞后系统极限环的自适应控制

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This paper reports the design of an online, dynamic, self-adjusting, neural network control methodology that will allow the neuron to add/drop to an optimum size during the identification of an unknown nonlinear hysteretic system responsible for the generation of limit cycle. Simultaneously, the identified model is used in the design of an adaptive control to suppress the limit cycle oscillation. Hysteresis is difficult to model or identify. The ensemble average concept based on the properties of the Preisach hysteresis model is used in the design of the neural networks during the network training phase. The radial basis function (RBF) networks employ two separate adaptation schemes where RBF's centers and width are adjusted by an extended Kalman filter, while the outer layer weights are updated using Lyapunov stability analysis to ensure the stable closed loop control. The effectiveness of the proposed dynamic neural control methodology is demonstrated through simulations to suppress the wing rock in the AFTI/F-16 test-bed aircraft having delta wing configuration.
机译:本文报告了一种在线,动态,自调整,神经网络控制方法的设计,该方法将允许神经元在识别导致极限循环的未知非线性磁滞系统的过程中增加/减少至最佳大小。同时,在自适应控制的设计中使用识别出的模型来抑制极限循环振荡。迟滞很难建模或识别。在网络训练阶段,基于Preisach磁滞模型属性的整体平均概念被用于神经网络的设计中。径向基函数(RBF)网络采用两种独立的自适应方案,其中RBF的中心和宽度通过扩展的Kalman滤波器进行调整,而外层权重则使用Lyapunov稳定性分析进行更新以确保稳定的闭环控制。通过仿真证明了抑制具有三角翼配置的AFTI / F-16试验台飞机的机翼岩石的有效性,从而证明了所提出的动态神经控制方法的有效性。

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