Trajectory Determination of Chang’E-5 during Landing and Ascending

Trajectory Determination of Chang’E-5 during Landing and Ascending

Chang’E-5 (CE-5) is China’s first lunar sample return mission. This paper focuses on the trajectory determination of the CE-5 lander and ascender during the landing and ascending phases, and the positioning of the CE-5 lander on the Moon. Based on the kinematic statistical orbit determination method...

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Bibliographic Details
Main Authors: Peng Yang, Yong Huang, Peijia Li, Siyu Liu, Quan Shan, Weimin Zheng
Format: Article
Language:English
Published: MDPI AG 2021-11-01
Series:Remote Sensing
Subjects:
Chang’E-5
sampling return
power landing
ascending
lander positioning
Online Access:https://www.mdpi.com/2072-4292/13/23/4837

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