The Orbit Design and Control Strategy of The Soft Landing of Chang 'e 3

DOI

10.2991/icismme-15.2015.438How to use a DOI?

Keywords

the soft landing; the Hermite interpolation method; the newton interpolation

Abstract

In this paper, we solve the problem of the orbit design and control strategy of the soft landing of Chang’e 3,Use the Hermite interpolation method and the Parabolic interpolation method to analyze each stage of the process.By using the interpolation method in numerical analysis, which based on the theory of kinematics and mechanics knowledge, with the help of the Realization of matlab sortware to solve the problem.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yan Yao
AU  - Yingbing Fan
AU  - Xiaocheng Gao
PY  - 2015/07
DA  - 2015/07
TI  - The Orbit Design and Control Strategy of The Soft Landing of Chang 'e 3
BT  - Proceedings of the First International Conference on Information Sciences, Machinery, Materials and Energy
PB  - Atlantis Press
SP  - 2110
EP  - 2113
SN  - 1951-6851
UR  - https://doi.org/10.2991/icismme-15.2015.438
DO  - 10.2991/icismme-15.2015.438
ID  - Yao2015/07
ER  -