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基于MATLAB/Simulink的火箭飞行故障仿真
引用本文:程龙,蔡远文,穆利军,任江涛.基于MATLAB/Simulink的火箭飞行故障仿真[J].兵工自动化,2008,27(9):8-11.
作者姓名:程龙  蔡远文  穆利军  任江涛
作者单位:1. 装备指挥技术学院,研究生1队,北京,101416;装备指挥技术学院,航天装备系,北京,101416
2. 装备指挥技术学院,航天装备系,北京,101416
3. 装备指挥技术学院,71315部队,河南,商丘,476000
4. 装备指挥技术学院,研究生1队,北京,101416
摘    要:对火箭的飞行故障进行仿真,有利于改进系统设计、提高可靠性,并为故障的诊断与隔离提供参考与支持。对火箭飞行仿真体系结构框架进行了设计。并基于MATLAB/Simulink仿真环境,实现全过程飞行仿真,给出仿真的流程。最后,以动力系统故障为例进行了故障仿真,并与正常情况进行了对比,结果合理。

关 键 词:运载火箭  飞行  MATLAB/SIMULINK  故障  仿真

Fault Simulation of Launch Vehicle Flight Based on MATLAB/Simulink
CHENG Long,CAI Yuan-wen,MU Li-jun,REN Jiang-tao.Fault Simulation of Launch Vehicle Flight Based on MATLAB/Simulink[J].Ordnance Industry Automation,2008,27(9):8-11.
Authors:CHENG Long  CAI Yuan-wen  MU Li-jun  REN Jiang-tao
Affiliation:CHENG Long, CAI Yuan-wen, MU Li-jun, REN Jiang-tao (1. No.1 Brigade of Graduate, Institute of Command & Technology of Equipment, Beijing 101416, China; 2. Dept. of Spaceflight Equipment, Institute of Command & Technology of Equipment, Beijing 101416, China; 3. No. 71315 Unit of PLA, Shangqiu 476000, China)
Abstract:The simulation of faults during the flight of the launch vehicle is good for system design, while can increase the reliability, and support its fault diagnosis and isolation. Structural framework of the simulation system is designed. The whole process simulation of flight is realized based on MATLAB/Simulink, and the process of simulation is introduced. Finally, taking faults in the dynamic system as an example, a fault simulation is performed. The result proved to be reasonable by compared with that under normal conditions.
Keywords:Launch vehicle  Flight  MATLAB/Simulink  Fault  Simulation
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