@inproceedings{e7cd9590491a4e27b73df1b2fe5629b3,
title = "Fast design and optimization of the low energy lunar escaping trajectory",
abstract = "In this paper, a fast design and optimizing method of the low energy lunar escaping trajectory is introduced in the earth-moon elliptical four body system. Firstly, to find the optimal escaping conditions rapidly, the energy demand of the spacecraft is analyzed and it's found that when Moon is getting near its perigee and Sun becomes co-linear with Earth and Moon the escaping will consume the least amount of fuel. Then, given the appropriate launching opportunity the Manifold Degeneration Method is introduced to optimize the escaping energy. Finally, the computing process of the escaping trajectory design and optimization which contains 5 steps is given. According to the simulation results, the computing process proposed is effective in searching the optimal escaping trajectory and over 25\% of the launching impulse can be saved with the optimal escaping orbit.",
keywords = "Design, Fast, Low Energy, Moon Escaping, Optimization",
author = "Yue Liu and Yingjing Qian and Wuxing Jing",
note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 28th Chinese Control and Decision Conference, CCDC 2016 ; Conference date: 28-05-2016 Through 30-05-2016",
year = "2016",
month = aug,
day = "3",
doi = "10.1109/CCDC.2016.7531167",
language = "英语",
series = "Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1203--1208",
booktitle = "Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016",
address = "美国",
}