第21卷
第5期
2013年5月
1004-924X(2013)05-1258-07
文章编号
光学精密工程
Optics and Precision Engineering
飞行器虚拟振动试验平台构建刘源1，董立珉1*，孔宪仁1，王日昆，李霖圣（1.哈尔滨工业大学航天学院，黑龙江哈尔滨150001；
2.上海航天卫星总装试验部，上海201109）
Vol.21No.5
May2013
摘要：针对用振动台进行飞行器振动环境试验时存在试验周期长、耗费高及易发生过试验或欠试验等问题，采用虚拟现实技术建立了飞行器虚拟振动试验平台。采用系统仿真软件LMSAMESim建立了电振动台正弦振动控制仪模型；通过多学科系统伤真软件LMSVirtual.Lab建立了振动台的多体系统动力学模型，进行了振动台多体动力学模型与电磁作动系统模型的机电联合仿真；实现了振动控制系统、电磁作动系统、振动台与试件机械系统的闭环伤真，构建了飞行器虚拟振动试验平台。利用该虚拟振动试验平台系统进行了盒式试件的正弦振动试验。结果表明，采用机电耦合建模方法构建的虚拟振动试验平台综合考虑了试件、振动台机械系统、控制系统及电气系统的耦合效应，可为飞行器的试前分析和虚拟振动试验提供试验环境。
关键调：飞行署设计；振动试验；机电联合仿真振动台
中图分类号：V416.2
文献标识码：A
doi;10,3788/OPE,20132105.1258
Constructionof virtualvibrationtestingplatformfor
spacecraft
LIU Yuan', DONG Li-min'', KONG Xian-ren', WANG Ri-kun', LI Lin-sheng(l.SchoolofAstronautics,HarbinInstituteofTechnology,Harbin150oo1,China; 2.ShanghaiAssemblyTestDepartmentofAerospaceSatellite,Shanghai201109,China)
*Correspondingauthor，E-mail:1010520507@163.com
Abstract: As the spacecraft vibration testing based on a shaking table has some defects, such as long time cycle, high cost, easy to produce over-testing and under-testing, a virtual vibration testing plat-form was built based on virtual reality technology. A sine vibration controller model of the electrical vibration table was built by system simulation software LMS AMESim and a multi-body model for the vibration table was established based on the multi-body simulation software LMS Virtual. Lab Mo-tion. Furthermore, the model of electromagnetic actuator in the vibration testing system was realized using the simulation software LMS AMESim, and the co-simulation of vibration testing system was carried out by uniting the multi-body model and LMS AMESim model. In combination of the vibration control system, electromagnetic actuation system and shaking table test mechanical system, the whole
收稿日期：2012-11-18；修订日期：2012-12-25.
基金项目：国家自然科学基金资助项目（No.60704020)；中国博士后科学基金资助项目（No.2012M510971)；黑龙
江省博士后基金资助项目（No.LBH-Z11185)；中央高校基本科研业务费专项资金资助项目（No.HIT NSRIF.2014027)