某巡航式飞行器控制系统设计与仿真

The Design and Simulation of A Cruise Aircraft Control System

在详细分析某巡航式飞行器运动模型的基础上 ,论述了采用经典控制理论设计该飞行器控制系统的方法 ,并在考虑限幅、延迟等非线性环节的基础上 ,进一步对控制系统参数进行了仿真分析。通过部分仿真结果曲线可以看出 ,控制系统结构和参数合理 ,可以满足该飞行器控制的总体性能要求。同时 。

This paper mainly describes the method of designing a aircraft control system based on the classical control theory after creating the aircraft movement models. The control system's performance is also simulated with the effects of some nonlinear elements such as saturation and transport delay. From the results we can see that the structure and parameters are reasonable, the performance can meet the need of the task. At the same time, it can offer more creditable data and diagram for the hardware in the loop simulation and the flight experiment.