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推力矢量喷管控制系统的数字仿真研究
引用本文:刘文兴.推力矢量喷管控制系统的数字仿真研究[J].航空发动机,2010,36(4):6-7,5.
作者姓名:刘文兴
作者单位:沈阳发动机设计研究所,沈阳,110015
摘    要:结合某型发动机推力矢量喷管研制的实际工作,确定了轴对称推力矢量喷管的控制方案,建立了轴对称推力矢量喷管控制系统的数学模型,对此作了数字仿真研究。仿真结果表明:某型发动机推力矢量喷管控制方案是可行的,可满足发动机的性能要求。

关 键 词:喷管  推力矢量  控制  数字仿真

Digital Simulation Research of Control System for Thrust Vectoring Nozzle
Authors:LIU Wen-xing
Institution:LIU Wen-xing (Shenyang Aeroengine Research Institute, Shenyang 110015, China)
Abstract:Combining with the development of thrust vectoring nozzle for an engine, the control schema of an axisymmetric thrust vectoring nozzle was defined. The mathematical model of control system for the axisymmetric thrust vectoring nozzle was constructed, and digital simulation for the thrust vectoring nozzle was performed. The results show that the control schema of thrust vectoring nozzle for an engine is viable, and can meet the performance requirements of engine.
Keywords:nozzle  thrust vectoring  control  digital simulation
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