飞轮隔振平台组合系统的动力学建模  

Dynamic modeling of combined reaction wheel and vibration isolation platform system

作　　者：黄庭轩[1] 张尧[1] 徐世杰[1] 

机构地区：[1]北京航空航天大学宇航学院,北京100191

出　　处：《北京航空航天大学学报》2013年第1期120-125,共6页Journal of Beijing University of Aeronautics and Astronautics

基　　金：国家自然科学基金资助项目(10902003);研究生科技创新实践基金资助项目(YCSJ-01-201204)

摘　　要：为分析隔振平台对星上飞轮扰动的衰减效果,研究了飞轮隔振平台组合系统的动力学建模问题.首先推导出含有静动不平衡量的飞轮加隔振平台组合系统的动力学模型.从模型中得出,飞轮和平台之间存在耦合;转子的静动不平衡会体现为飞轮的多项扰动力和扰动力矩.其次,对这些扰动项进行量级分析,并据此简化系统方程.最后利用数值仿真将简化模型与之前的完整模型作对比,验证了此简化模型的合理性;并通过初步的整星系统仿真,说明了隔振系统对航天器姿态稳定度的改善效果.To analyze the attenuation effect of vibration isolation platform for reaction wheel （RW） dis- turbances, the dynamic modeling problem of the combined system which includes an imbalance RW and a pas- sive Stewart platform with kinetic base platform was studied. The precise dynamics formulation was derived. The equations show that there are coupling effects between the RW and the platform, and rotor imbalance can also produce additional coupling disturbances other than tonal disturbances. The magnitudes of these disturb- ances were investigated and a reduction of the system model was made accordingly. Numerical simulations were conducted to compare the reduced system model to the complete one, which check the validity of the re- duced model. And a primary simulation for whole spacecraft system shows that the vibration isolation system could improve the attitude stability effectively.

关 键 词：飞轮 隔振平台 静动不平衡 动力学建模 

分 类 号：V412.4[航空宇航科学与技术—航空宇航推进理论与工程]