飞机突防飞行非线性解耦控制的实时仿真实现

非线性解耦控制系统仿真是当前研究的重要方向之一。本文提出了一个仿真飞机在大气扰动下突防飞行非线性解耦控制的简便方法，该法用飞机指令变量的跟踪特性仿真系统的解耦控制特性和对期望突防航迹的跟踪特性，具有方法简单、易实现，计算稳定，实时性较好，结果准确、直观等特点，可用于设计、选择控制规律参数，研究和检验飞行器纵横向运动非线性交叉耦合的解耦控制特性，也可用于其它非线性解耦控制系统的实时仿真研究。

Real-Time Simulation Implementation of Nonlinear Decoupling Control for Aircraft Penetration Flight

This paper proposes a kind of simple method of simulating nonlinear decoupling coutrolfor aircraft TF/TA penetration flight in atmospheric disturbance,which can implement systemsimulation of decoupling control behavior and accurately capturing three-dimensional penetration trajec-tory by using capturing behavior of command variables,The method has a number of features,such asstable and accurate simulation computing and Good real- time simulation velocity,and also has the ad- vantages of being easy to use and easy implementation etc.It is a practical method.