摘要
针对航天器双主动交会问题,以两航天器能量消耗之和最小为最优交会指标,建立了一种寻求远程导引可行飞行方案的算法模型,以满足远程导引对测控、日照和任务时间等要求。仿真结果表明,该算法可行。
In order to implement the space cooperative rendezvous that were satisfied with the requirements of TT＆C, solar illumination and mission time, the algorithm for seeking feasible project of remote guidance in this paper, while the energy of the two spacecrafts consumed least was served as the optimal target. The simulation results showed that this algorithm was practicable.
出处
《上海航天》
北大核心
2007年第6期10-13,共4页
Aerospace Shanghai
