A Soft Landing Trajectory Design and Control Strategy

DOI

10.2991/icimm-15.2015.267How to use a DOI?

Keywords

Chang' e 3; soft landing; trajectory design; optimum control.

Abstract

This paper aims at realizing a soft landing of Chang' e 3 in a predetermined region on the moon. In line with the principle of low cost and business-friendly. It according to the scheduled landing point and combines with the actual operation of the Chang' e 3’s track to put forward the scheme of ‘safe radius spiral search algorithm’ and finally gives the landing trajectory and optimal control strategy.

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  - Haiyan Xuan
AU  - Yan Sun
AU  - Peijian Yan
AU  - Shaofei Dong
AU  - Panhong Zhao
PY  - 2015/07
DA  - 2015/07
TI  - A Soft Landing Trajectory Design and Control Strategy
BT  - Proceedings of the 5th International Conference on Information Engineering for Mechanics and Materials
PB  - Atlantis Press
SP  - 1466
EP  - 1469
SN  - 2352-5401
UR  - https://doi.org/10.2991/icimm-15.2015.267
DO  - 10.2991/icimm-15.2015.267
ID  - Xuan2015/07
ER  -