摘要
以飞机环境控制系统(AECS)为研究对象,建立了系统各主要部件的数学模型,对系统进行了仿真研究。采用模块化结构的方法,利用Matlab/Simulink建立各部件的仿真模块并构成系统进行仿真研究,对系统在扰动下的动态响应进行了仿真分析。仿真结果表明所建模型具有较高的精度,为研究飞机环境控制系统的动态性能提供了新的实现途径。
the whole aircraft environment control system (AECS) is researched. According to the working principle, the components' mathematical model of an aircraft environmental control system are set up. Using software Matlab/Simulink, the dynamic simulation of AECS has been made. The simulation results of this system indicate that the models has high-precision. This model provides a new approach to study the dynamic characteristics of aircraft environmental control system. It is of significance for designing and optimizing aircraft environmental control system.
出处
《计算机测量与控制》
CSCD
2005年第6期542-544,共3页
Computer Measurement &Control
