摘要
基于Matlab/Simulink软件开发平台,建立了冲压发动机控制系统的数学模型,通过TLC将仿真模型自动转化成C代码,提高仿真速度,并利用Real-Time Windows Target实现了仿真软件的实时运行。利用该仿真软件,实现了冲压发动机控制系统半实物仿真试验,对冲压发动机的供油控制规律进行仿真研究,验证了所采用的控制规律、控制算法的可行性。
Based on Matlab/Simulink developing platform, the ramjet control system mathematical model was developed. Simulation model was transformed into C code by TLC and the computing rate was improved, also real time operating of the simulation software was obtained by using Real- Time Windows Ramjet Target. Semi-physical simulation test for ramjet engine control system was conducted with this simulation software. The control law and methods were proved feasible through ramjet fuel supply law simulation study.
出处
《火箭推进》
CAS
2008年第5期49-53,共5页
Journal of Rocket Propulsion
