飞机前轮转弯系统仿真建模与分析

Modeling and Analysis of Aircraft Nose Wheel Steering Control System

基于一般飞机前轮转弯系统的组成及其工作原理，采用模块化建模的方法，建立了前轮转弯控制系统仿真模型。设置仿真初始条件，对所建立的模型进行仿真验证和分析。所建立的前轮转弯控制系统仿真模型具有可重复利用、便于修改和扩展等优点，可作为前轮转弯控制系统设计工具用于系统开发工作，也可直接应用于工程模拟器等仿真平台。

Based on the common structure and basic principles, the nose wheel steering model was established using the modularization design method. The simulation model was validated and analyzed by setting the initial simulation conditions. The nose wheel steering control system founded has the benefits of being reasable, easy to modify and expand, and can be used as a system design tool, and can also be directly applied to a engineer- ing simulator.