飞机外挂可靠性试验中MIMO振动响应控制仿真研究  

Simulation of MIMO vibration response control in the reliability test of aircraft store

作　　者：王光芦[1] 徐明[1] 

机构地区：[1]中国航空综合技术研究所,北京100028

出　　处：《航天器环境工程》2009年第1期51-55,6-7,共5页Spacecraft Environment Engineering

摘　　要：文章阐述了飞机外挂MIMO(多输入多输出)振动响应控制仿真的目的、仿真模型和程序,并将该技术应用于某型号外挂设计定型可靠性鉴定试验。通过对多种控制方案进行仿真比较,确定出最佳控制方案,顺利完成了某型号外挂设计定型可靠性鉴定试验。The paper discusses the simulation of MIMO(Multi-Input-Multi-Output) vibration response,including the purpose,the model and the procedure.The simulation technology is used in some aircraft store reliability tests.The optimal control scheme is obtained by comparing the simulation results of many control schemes.Based on the best control scheme,some aircraft store reliability test was successfully carried out.

关 键 词：振动 响应控制 可靠性试验 飞机外挂 仿真 

分 类 号：V241.01[航空宇航科学与技术—飞行器设计]