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基于Simulink/RTW的冲压发动机控制系统半实物仿真
引用本文:尤裕荣,徐中节,逯婉若. 基于Simulink/RTW的冲压发动机控制系统半实物仿真[J]. 火箭推进, 2008, 34(5): 49-53
作者姓名:尤裕荣  徐中节  逯婉若
作者单位:西安航天动力研究所,陕西,西安,710100
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。

关 键 词:Simulink/RTW  冲压发动机控制系统  半实物仿真

Semi-physical simulation on ramjet control system based on simulink/RTW
You Yurong,Xu Zhongjie,Lu Wanruo. Semi-physical simulation on ramjet control system based on simulink/RTW[J]. Journal of Rocket Propulsion, 2008, 34(5): 49-53
Authors:You Yurong  Xu Zhongjie  Lu Wanruo
Affiliation:You Yurong,Xu Zhongjie,Lu Wanruo (Xi'an Aerospace Propulsion Institute,Xi'an 710100,China)
Abstract: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 RealTime 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.
Keywords:Simulink/RTW
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