环月远程快速交会任务规划  

Mission Planning of Fast Rendezvous Strategy around the Moon

作　　者：陈欢[1] 张洪礼[1] 韩潮[1] 彭坤[2] 马晓兵[2] 胡雯婷[3] 

机构地区：[1]北京航空航天大学,北京100191 [2]中国空间技术研究院载人航天总体部,北京100094 [3]北京机电工程研究所,北京100074

出　　处：《载人航天》2016年第4期417-422,共6页Manned Spaceflight

基　　金：载人航天预先研究项目(010103)

摘　　要：针对载人登月返回任务中月面上升舱与指挥服务舱的环月远程快速交会问题,以共椭圆快速交会策略为标称策略,并给出摄动模型下的修正方法。给出考虑总交会时间约束、机动时间间隔约束和燃料优化效率的燃料最优共椭圆快速交会策略,以及考虑总速度增量约束、机动时间间隔约束和时间优化效率的时间最优共椭圆快速交会策略。通过算例仿真验证了共椭圆快速交会策略的可行性以及摄动模型下的交会精度,对共椭圆快速交会策略的总速度增量与交会时间的关系进行分析,并对比燃料最优和时间最优共椭圆快速交会对接策略,证明了优化策略的有效性。Co-ellipse fast rendezvous strategy was presented as the standard strategy for the remote rendezvous between the lunar module and the command and service module around the moon in a manned landing and return mission. Fuel-optimal co-ellipse fast rendezvous strategy considering the constraints of total rendezvous time,maneuver time interval and fuel-optimal efficiency,and timeoptimal co-ellipse fast rendezvous strategy considering the constraints of total velocity increment,maneuver time interval and time-optimal efficiency,were introduced. Several numerical simulations were conducted to test the feasibility and precision of the standard,fuel-optimal and time-optimal coellipse rendezvous strategies. Analysis of the relationship between the total velocity increment and the rendezvous time was also conducted to confirm the feasibility of the optimal strategies.

关 键 词：环月远程交会 快速交会 共椭圆交会 燃料最优 时间最优 

分 类 号：V412.4[航空宇航科学与技术—航空宇航推进理论与工程]