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Design and Calculation of the Landing Track Preparation of Chang'e-3 Probe
2016
Proceedings of the 2016 Joint International Information Technology, Mechanical and Electronic Engineering
unpublished
This paper discussed the problems in the soft landing of Chang'e-3 Probe on moon, established a Selenocentric celestial coordinate system, used the latitude and longitude coordinates coefficients conversion formula, calculated the location of the perilune and the apolune of Chang'e-3 soft landing. The author divided the landing process into five stages: main decelerating phase, fast adjustment phase, crude avoidance phase, fine avoidance stage and free fall process. By using Newton movement
doi:10.2991/jimec-16.2016.104
fatcat:7kg446chfnchffogbsgnnofigy