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对执行器动力学具有鲁棒性的吸气式高超声速飞行器的神经自适应控制

Neural adaptive control of air-breathing hypersonic vehicles robust to actuator dynamics.

作者信息

An Hao, Guo Ziyi, Wang Guan, Wang Changhong

机构信息

Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin, 150001, PR China.

出版信息

ISA Trans. 2021 Oct;116:17-29. doi: 10.1016/j.isatra.2021.01.017. Epub 2021 Jan 11.

Abstract

This paper investigates the neural adaptive control problem for air-breathing hypersonic vehicles. For the velocity subsystem, a radial basis function neural network (RBFNN)-based adaptive controller is first designed, which employs the auxiliary variable to compensate for the saturation nonlinearity of the scramjet control command. For the altitude subsystem, an RBFNN-based controller addresses actuator constraints and dynamics using the model predictive control, as well as counteracts uncertainties and disturbances using the neural adaptive mechanism. The effectiveness of the proposed control is verified by simulations.

摘要

本文研究吸气式高超声速飞行器的神经自适应控制问题。对于速度子系统,首先设计了一种基于径向基函数神经网络(RBFNN)的自适应控制器,该控制器采用辅助变量来补偿超燃冲压发动机控制指令的饱和非线性。对于高度子系统,基于RBFNN的控制器利用模型预测控制来处理执行器约束和动力学问题,并利用神经自适应机制抵消不确定性和干扰。通过仿真验证了所提控制方法的有效性。

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