国防科技大学学报2011，Vol.33Issue(4)：6-11,6.
探月飞行器定点返回轨迹特性分析
Point Return Trajectory Characteristics Analysis for a Lunar Spacecraft
摘要
Abstract
The point return orbit characteristics for a vehicle from a lunar mission were studied, and how the landing point and reentry point vary was focused upon. Firstly, analysis of some characteristic points was presented, and lunar anb'pode, reentry point and perigee were included. Tnen the stabilization property of the latitude and velocity at reentry point was achieved. Furthermore, baaed on the characteristics of the foregoing three points, approximate method for the theoretical relation of landing point and reentry point was proposed. In addition, relation of lighting condition at landing point and lunar return window was analyzed by using lunar phase law, and die basic conclusions was attained qualitatively. Finally, the orbit simulation was established with double two-body model, which shows the feasibility of this theoretical model in predicting the lunar point return orbit.关键词
月球探测/定点返回/轨迹特性/月球反垂点/返回窗口Key words
moon exploration/ point return/ orbit characteristics/ lunar artipode/ return window分类
航空航天引用本文复制引用
沈红新,李海阳,彭祺擘,杜昕..探月飞行器定点返回轨迹特性分析[J].国防科技大学学报,2011,33(4):6-11,6.基金项目
国家自然科学基金资助项目(10902121) （10902121）
