云南高校图书馆联盟文献共享服务平台- LUNAR

LUNAR: 作品数：430被引量：593H指数：13; 导出分析报告; 相关领域：天文地球医药卫生更多>>; 相关作者：张影从中华王闯管文敏夏维波更多>>; 相关机构：武汉大学哈尔滨工业大学北京航空航天大学首都医科大学附属北京佑安医院更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家高技术研究发展计划国家重点基础研究发展计划国家教育部博士点基金更多>>

SCIENCE AND TECHNOLOGY: 《China Today》2024年第5期69-69,共1页; China's Queqiao-2 Relay Satellite Enters Lunar Orbit China's Queqiao-2 relay satellite has successfully performed a near-moon braking procedure and entered its circumlunar orbit,according to the China National Space A...; 关键词：BRAKING LUNAR ORBIT

Fast solution to the free return orbit's reachable domain of the manned lunar mission by deep neural network被引量：1: 《Journal of Systems Engineering and Electronics》2024年第2期495-508,共14页YANG Luyi LI Haiyang ZHANG Jin ZHU Yuehe; supported by the National Natural Science Foundation of China (12072365);the Natural Science Foundation of Hunan Province of China (2020JJ4657)。; It is important to calculate the reachable domain(RD)of the manned lunar mission to evaluate whether a lunar landing site could be reached by the spacecraft. In this paper, the RD of free return orbits is quickly eval...; 关键词：manned lunar mission free return orbit reachable domain(RD) deep neural network computation efficiency

Two-maneuver indirect contingency return from a low lunar orbit被引量：1: 《Chinese Journal of Aeronautics》2023年第8期115-127,共13页Yunfei LI Xiaosheng XIN Xiyun HOU; supported by the National Natural Science Foundation of China(No.12233003).; The problem of contingency return from the low lunar orbit is studied.A novel twomaneuver indirect return strategy is proposed.By effectively using the Earth’s gravity to change the orbital plane of the transfer orbi...; 关键词：MOON Lowlunarorbit Contingencyreturn Third-body maneuver Gravityassist

Influence of Lunar Orbit Variation on Global Climate and Environment: 《Journal of Environmental Science and Engineering(B)》2022年第4期91-96,共6页Cuixiang Zhong; Twenty four solar terms summarized by people through long-term observation of the sun’s annual activity has roughly revealed the changing laws of seasons,climate,phenology and so on in a year,reflecting the impact of...; 关键词：Glacial retreat lunar activity global climate warming environmental change COUNTERMEASURE

Shape and position of Earth's bow shock near-lunar orbit based on ARTEMIS data被引量：4: 《Science China Earth Sciences》2016年第8期1700-1706,共7页LIU Ji SHI QuanQi TIAN AnMin Lü JianYong WU Hao WANG Ming FU SuiYan YANG YuChen ZONG QiuGang ZHANG Jiang FENG YongYong PU ZuYin; supported by the National Natural Science Foundation of China(Grant Nos.41322031,41404131,41574157,41031065&41304129);the Specialized Research Fund for State Key Laboratories;the Shandong Natural Science Foundation(Grant Nos.2013BSE27132,BS2013HZ001); Earth's bow shock is the result of interaction between the supersonic solar wind and Earth's magnetopause. However, data limitations mean the model of the shape and position of the bow shock are based largely on near-...; 关键词：Bow shock Interplanetary magnetic field(IMF) MAGNETOSPHERE Solar wind

Design of low-energy transfer from lunar orbit to asteroid in the Sun-Earth-Moon system: 《Acta Mechanica Sinica》2014年第6期966-972,共7页Ya-Min Wang Dong Qiao Ping-Yuan Cui; supported by the National Basic Research Programof China(973 Program)(2012CB720000);the National Natural Science Foundation of China(11102020);Program for New Century Excellent Talents in University;Beijing Higher Education Young Elite Teacher Project and China Scholarship Council; Asteroid exploration trajectories which start from a lunar orbit are investigated in this work.It is assumed that the probe departs from lunar orbit and returns to the vicinity of Earth,then escapes from the Earth by ...; 关键词：Lunar orbit Asteroid exploration Low-energy transfer Sun-Earth-Moon system

Double lunar swing-by orbits revisited: 《Science China(Physics,Mechanics & Astronomy)》2014年第4期784-790,共7页HOU XiYun LIU Lin; supported by the National Natural Science Foundation of China(Grant No.10903002); The double lunar swing-by orbits are a special kind of orbits in the Earth-Moon system.These orbits repeatedly pass through the vicinity of the Moon and change their shapes due to the Moon’s gravity.In the synodic fr...; 关键词：double lunar swing-by orbit restricted three-body problem periodic orbit

Statistical study of the properties of the magnetic field and plasma in the earth's magnetotail near lunar orbit被引量：5: 《Science China(Technological Sciences)》2012年第9期2570-2577,共8页TIAN Tian ZONG QiuGang WANG YongFu FEI ZengPing; supported by the National Natural Science Foundation ofChina (Grant No. 40831061);the National Key Laboratory Special Fund and the Open Research Foundation of Science and Technology on Aerospace Flight Dynamics Laboratory (Grant No. 2012afd1034); Based on the magnetic field and plasma data obtained by GEOTAIL in 1992-1995 and WIND in1994-2009, the magnetic field and plasma properties in the magnetotail near lunar orbit were studied statistically using the supe...; 关键词：LUNAR space weather PLASMA current sheet STORM superposed epoch analysis

Free return orbit design and characteristics analysis for manned lunar mission被引量：24: 《Science China(Technological Sciences)》2011年第12期3243-3250,共8页PENG QiBo SHEN HongXin LI HaiYang; supported by the National Natural Science Foundation of China (Grant No.10902121); A circumlunar free return orbit design model that satisfies manned lunar mission constraints is established. By combining analytical method with numerical method,a serial orbit design strategy from initial value desig...; 关键词：manned lunar mission free return orbit orbit design orbit characters

Solution space analysis of Double Lunar-Swingby periodic trajectory被引量：2: 《Science China(Technological Sciences)》2010年第8期2081-2088,共8页LUO ZongFu ,MENG YunHe&TANG GuoJian College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073,China; supported by the National Natural Science Foundation of China(Grant No.10702078);the Pre-research Foundation of National University of Defense Technology(Grant No.JC08-01-05); The Double Lunar-Swingby(DLS)periodic trajectory is a type of large-scale trajectory in Restricted Three-Body Problem framework.First,the principium of the DLS periodic trajectory is studied,and a preliminary design o...; 关键词：DOUBLE Lunar-Swingby patched CONICS SOLUTION space analysis ORBIT design PERIODIC ORBIT

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