Dynamics analysis and the attitude prediction of the spacecraft were realized by using the knowledge of dynamics and virtual prototyping technology, and the results of theoretical calculations and ADAMS emulation were compared to verify the correctness of the model. At the same time, the factors and fault influencing the attitude of a spacecraft were considered to get the results of separation. Using the ADAMS software for spacecraft ground simulation can avoid the complex dynamics calculation, and has the widespread application prospect.
参考文献
相似文献
引证文献
引用本文
卢丽颖,孟宪红,邢依琳.卫星空间分离动力学研究[J].动力学与控制学报,2014,12(2):165~169; Lu Liying, Meng Xianhong, Xing Yilin. Dynamic study of satellite space separation[J]. Journal of Dynamics and Control,2014,12(2):165-169.