Phasing Orbit Design and Flight Test of Lunar Orbit RVD in Chang'e-5 Mission

被引：0
|
作者：
Wang Z.-S. [1 ]
Meng Z.-F. [1 ]
Gao S. [1 ]
Peng J. [1 ]
机构：
[1] Beijing Institute of Spacecraft System Engineering, Beijing
来源：
Yuhang Xuebao/Journal of Astronautics | 2021年 / 42卷 / 08期
关键词：
Chang'e-5; Lunar orbit; Phasing orbit design; Rendezvous and docking;
D O I：
10.3873/j.issn.1000-1328.2021.08.001
中图分类号：
学科分类号：
摘要：
The phasing orbit design of the lunar orbit rendezvous and docking operation in Chang'e-5 mission is discussed in the paper, with consideration of the uniqueness of lunar orbit rendezvous and docking missions and the practical engineering constraints of China Lunar Exploration Program. The paper addresses the two aspects of the phasing orbit design, namely the phasing orbit designs of the ascent module and the orbiter, with the focuses on the multi-impulse orbit scheme selection, nominal orbit optimization, orbit control strategy and error analysis.Moreover, the actual flight data of Chang'e-5 mission is provided to verify the correctness of the designs. © 2021, Editorial Dept. of JA. All right reserved.
引用
收藏
页码：939 / 952
页数：13
相关论文
共 24 条
  • [1] Zhu Ren-zhang, Wang Hong-fang, Cong Yun-tian, Et al., Comparative study of Chinese and foreign rendezvous and docking technologies, Spacecraft Engineering, 22, 3, pp. 8-15, (2013)
  • [2] Zhu Ren-zhang, Wang Hong-fang, Xu Yu-jie, Et al., Study on rendezvous techniques of American spacecraft, Spacecraft Engineering, 20, 5, pp. 11-36, (2011)
  • [3] Wu Hong-xin, Hu Hai-xia, Xie Yong-chun, Et al., Several questions on autonomous rendezvous docking, Journal of Astronautics, 24, 2, pp. 132-137, (2003)
  • [4] Wang Zhong-gui, Design and flight test of the far-range guidance scheme of china's first space rendezvous and docking mission, SCIENTIA SINICA Technologica, 42, 7, pp. 764-770, (2012)
  • [5] Zhang Jin, The phasing maneuver strategy planning for space rendezvous missions, (2008)
  • [6] (2008)
  • [7] Alexander J D, Becker R W., Apollo experience report-evolution of the rendezvous maneuver plan for lunar landing missions, (1973)
  • [8] Sostaric R R, Merriam R S., Lunar ascent and rendezvous trajectory design, The 31st Annual AAS Guidance and Control Conference, (2008)
  • [9] Lee A Y, Ely T, Sostaric R, Et al., Overview of a preliminary design of the guidance, navigation, and control system of the Altair lunar lander, AIAA Guidance, Navigation, and Control Conference, (2010)
  • [10] D'Souza C, Crain T., Orion cislunar guidance and navigation, AIAA Guidance, Navigation, and Control Conference, (2007)
123