摘要
建立了绳系子卫星在有偏置情况下的动力学方程,并通过简化方程组深入讨论了绳系子卫星的展开策略及相应的运动特征。数值仿真结果证明这种展开策略是可行的。
The tethered satellite system is one of the hot points that have been studied inastronautics in America and some European countries for years. Agroup of dynamical equationshave been established in the presence of offset, and several deploying strategies and characteristicsof corresponding motion have been discussed in depth in this paper. Finally, the results ofsimulation show that which strategy is feasible.
出处
《哈尔滨工业大学学报》
EI
CAS
CSCD
北大核心
1998年第1期11-14,共4页
Journal of Harbin Institute of Technology
基金
国家自然科学基金