摘要
研究了基于Butterworth滤波器设计思想的控制器设计方法,将这种方法应用于某飞机纵向飞行控制的设计,并进行了鲁棒性仿真研究。结果表明:该方法设计简单,只需确定一个设计参数,就可对飞行控制系统进行初期阶段设计,具有较强的工程实用价值。
The controller design method based on a Butterworth filter is studied. This method is used to design a flight control system of aircraft. Robustness simulation results are given. The method is easy to design and only one design parameter needed. It can be used in earlier design of flight control systems and convenient for engineering implementation.
出处
《飞行力学》
CSCD
北大核心
2009年第1期74-76,96,共4页
Flight Dynamics
基金
西北工业大学科研启动基金资助项目(0500-06XE0121)
