嫦娥一号卫星的地月转移变轨控制

Abstract

Abstract: A highly reliable and accurate on-board control system design scheme is presented for the orbit maneuvers of CE-1 spacecraft during its cislunar transfer phase．Flight trajectories，orbit transfer strategies and parameter optimization，on—board autonomous maneuver control procedures and parameter caliberations are addressed．Flight verification results are given as well．

Key words:

font-family:Calibri, sans-serif, "> font-family:宋体, CE-1 spacecraft">CE-1 spacecraftfont-family:宋体, ')">">, cislunar transfer, orbit control, autonomous orbit maneuver

CLC Number:

V446．1

ZONG Hong, WANG Shuyi , HAN Dong, WANG Dayi , LI Tieshou, ZHANG Honghua , HUANG Jiangchuan. Orbit Maneuver Control during Cislunar-Transfer Phase for CE-1 Spacecraft[J].Aerospace Contrd and Application, 2008, 34(1): 44-50.

0
/ / Recommend CE-1 spacecraft；cislunar transfer；orbit control；autonomous orbit maneuver
”. Please open it by linking:https://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/abstract/abstract9384.shtml" name="neirong"> CE-1 spacecraft；cislunar transfer；orbit control；autonomous orbit maneuver
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Orbit Maneuver Control during Cislunar-Transfer Phase for CE-1 Spacecraft

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