An adaptive inverse controller for hypersonic vehicle

Jiaxue Liu, Qian Wang, ZengShuai Pan, Wei Wei
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引用次数: 1

Abstract

A neural network adaptive inverse controller structure is proposed to solve the problems that hypersonic aircraft with highly nonlinear and flight conditions of large span. OS-ELM algorithm is improved with RBF network for online learning and adaptive inverse controller for the online training is used. Hypersonic aircraft with six degrees of freedom non-linear model is used to verify the performance of adaptive inverse controller. The controller based on flight conditions doing online learning in real time is shown with flight simulation in a typical condition. Aircraft orders tracking is achieved rapidly and steadyly and desired control effect is achieved.
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高超声速飞行器自适应逆控制器
针对高超声速飞行器高度非线性和大跨度飞行条件的问题,提出了一种神经网络自适应逆控制器结构。对OS-ELM算法进行改进,采用RBF网络进行在线学习,并采用自适应逆控制器进行在线训练。采用六自由度高超声速飞行器非线性模型,验证了自适应逆控制器的性能。通过典型工况下的飞行仿真,展示了基于飞行工况的控制器实时在线学习。实现了飞机订单的快速稳定跟踪,取得了理想的控制效果。
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