Dynamic Inversion Based on Neural Network Applied to Nonlinear Flight Control System

摘要：

Modern flight control system is always a complicated nonlinear flight control system, this paper presents a control method of dynamic inversion based on neural network applied to nonlinear flight control system. Through analyzes the decoupling inversion and tracking principle of neural network, a dynamic neural network is presented, which consist of static neural network and integrators. Based on the dynamic neural network, a control method of dynamic inversion used for multi-variable nonlinear flight control system is designed, and simulation of flight control system of power parafoil is made. Simulation results demonstrate that the control method has strong ability of control and robustness.

关键词： dynamic inversion nonlinear system control neural network flight control system

作者: Kechang Qian Zili Chen

作者单位: Ordance Engineering College Shijiazhuang, China

会议类型: 国际会议

会议名称: The 2010 2nd International Conference on Future Computer and Communication(第二届未来计算机与通信国际会议 ICFCC 2010)

会议地点: 武汉

会议语种:英文

页码: 699-703

在线出版日期: 2010-05-21（万方平台首次上网日期，不代表论文的发表时间）