非线性飞行控制方法研究概述

AN INTRODUCTION TO NONLINEAEAR FLIGHT CONTROL

原理性地给出了目前常用的几种非线性飞行控制方法，即：数值优化法，动态逆设计方法，微分几何法和滑态变结构设计方法。指出了非线性飞行控制对提高战斗机机动性和敏捷性有重要作用，同时也介绍了这几种方法在非线性飞行控制中的应用情况。

A few rnethodlogies for nonlinear flight control law design are presentedin principle.They are numerical optimization techniques,nonlinear inversion dynamics,differential geometry theory and sliding state method.It is pointed out that the developmentof nonlinear flight control play an important role in augmenting fighter’s maneuverabilityand agility.The application of these methodlogies to nonlinear flight control is introducedalso.