【作者】 关鹏； 郭晶； 陆平；

【Author】 Guan Peng~1 Guo Jing~1 Lu Ping~2 (1 BACC - Beijing Aerospace Control Centre 100094) (2 College of Aerospace Aviation,Shanghai Jiaotong University 200240)

【机构】 北京航天飞行控制中心； 上海交通大学航空航天学院；

【摘要】 通过对载人空间站管理和载人登月任务需求的分析,研究了同时具备载人航天飞行与载人登月飞行相结合的任务工作模式。通过近地轨道和近月轨道的飞行模式设计,针对载人登月飞行、交会对接飞行、组合体飞行和空间站组合管理利用模式等,探讨了近地轨道、地月过渡轨道、环月轨道、登月飞行及返回等各个阶段的飞行模式问题。完成了不同飞行阶段的任务分析,提出了任务实施的难点和解决问题的思路,并从实际出发,探讨了适应本土特色的飞行模式设计,研究了飞行风险和研制可性性的综合因素,分析和评估了可行的飞行任务设计方法。针对现状设计了有限规模的发展模式,探讨了载人航天与探月工程合理交叉准备和基本飞行的试验方式。更多还原

【Abstract】 With the development of the manned space flight mission and lunar exploration project mission,the manned lunar mission will be the most necessary in these years.Studying the low earth orbit manned space station mission,low lunar orbit mission and the technology of orbit rendezvous etc.,it is designed that a new Flight Control Modes for Manned Lunar Mission with the way of limiting easy rocket.It is important and valuable that the flight test about human lunar mission can be tried and performed in no time.Because the different mission mode about the manned lunar flight will be able to require the dissimilar rocket capability and launch times,the design of the flight mission mode give the comparison about different spacecraft flight mission modes and analyze risk and estimate its practicable in restricted dimensions mode.Finally,further research needs in the mission would be designed in some optimization methodologies.更多还原