Control Method at Obstacle Avoidance Stage for Spacecraft

DOI

10.2991/cmes-15.2015.108How to use a DOI?

Keywords

Linear discrete, Iteration method, Genetic algorithm, Gray matrix. Matlab

Abstract

Based on the operation data and basic parameters of spacecraft, soft landing process is done reasonable simplification equivalent. Without losing the accuracy, this paper proposes the control scheme at obstacle avoidance stage. The landing preparation track is accord with the energy conservation and the Kepler's motion law. The control strategy of soft landing can use differential to solve the optimal control strategy using Newton classical mechanics law. It has a certain practical application value in the spacecraft landing parameters calculation and track design.

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  - Xueyuan Zhang
PY  - 2015/04
DA  - 2015/04
TI  - Control Method at Obstacle Avoidance Stage for Spacecraft
BT  - Proceedings of the 2nd International Conference on Civil, Materials and Environmental Sciences
PB  - Atlantis Press
SP  - 387
EP  - 390
SN  - 2352-5401
UR  - https://doi.org/10.2991/cmes-15.2015.108
DO  - 10.2991/cmes-15.2015.108
ID  - Zhang2015/04
ER  -