Design of Chang'e No.three Soft Landing Orbit Based on GA and Texture Analysis

DOI

10.2991/icismme-15.2015.418How to use a DOI?

Keywords

soft landing ;dynamic programming; genetic algorithm; texture analysis

Abstract

this paper the reduction of Chang'e no.3 soft landing and obstacle avoidance phase are studied. And based on that, there is an orbital control scheme with the aim of consumption the least fuel. In this scheme, the dynamic programming model that aims at consuming the least fuel is set up for the main reduction stage. Combined with the genetic algorithm, we get the optimal control scheme. During the obstacle avoidance phase, we use the texture analysis to quickly identify the surface imaging and automatically look for a safe landing area in order to avoid obstacle.

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  - Jiani Xing
PY  - 2015/07
DA  - 2015/07
TI  - Design of Chang'e No.three Soft Landing Orbit Based on GA and Texture Analysis
BT  - Proceedings of the First International Conference on Information Sciences, Machinery, Materials and Energy
PB  - Atlantis Press
SP  - 2026
EP  - 2030
SN  - 1951-6851
UR  - https://doi.org/10.2991/icismme-15.2015.418
DO  - 10.2991/icismme-15.2015.418
ID  - Xing2015/07
ER  -