摘要
建立卫星飞轮支架的有限元模型并进行了模态及响应计算,也对相关支架的有限元模型计算结果与实 验结果进行比较,进而探讨飞轮支架及其组件是否达到使用环境要求。在此基础上,对飞轮支架组件的模态与响应控制 的规律及如何控制进行若干分析。
The finite element model of satellitic flywheel-bracket-groupware is created and the mode and response analysis for the model is carried out. The result of calculation is compared with that of experiment and whether the flywheel-bracket-groupware comes up to the standard or not is discussed. With this understanding, the rule of mode and response control of flywheel-bracket-groupware and the control practice are presented.
出处
《振动与冲击》
EI
CSCD
北大核心
2005年第1期63-65,共3页
Journal of Vibration and Shock
