空间科学学报2012，Vol.32Issue(4)：550-554,5.
挠性航天器系统动力学耦合特性研究
Study on Dynamic Coupling Characteristic of Flexible Spacecraft
摘要
Abstract
Dynamic forward recursive formulation of rigid-flexible coupled multi-body system is an important modeling theory of dynamics, which will not only reduce the workload but also avoid the accumulated error. It is apt to the exact solution when applied to complex systems because it retains the influence caused by elastic vibration of flexible parts to the center of mass and moment of inertia. In this paper, the general type of forward recursive formulation to rigid-flexible coupled spacecraft system was applied, and the higher accuracy in calculation was expounded. Finally, through numerical calculation, advantage of the forward recursive method in handling the coupling of flexible system than that of the traditional method was verified.关键词
单向递推/耦合系数/挠性系统/动力学仿真Key words
Forward recursive formulation/Coupling coefficient/Flexible system/Dynamic simulation分类
航空航天引用本文复制引用
陆毓颖,刘铸永,洪嘉振..挠性航天器系统动力学耦合特性研究[J].空间科学学报,2012,32(4):550-554,5.基金项目
博士点基金项目（20090073110009）和上海市自然科学基金项目（11ZRl417000）共同资助 （）
