Physical Simulation Experiment System of Multi-Rigid-Body Spacecraft Attitude Control Based on Micro-Gravity Floating Platform Environment

DOI

10.2991/jimet-15.2015.197How to use a DOI?

Keywords

multi-rigid-body spacecraft, flotation units, real-time simulation, virtual instrument

Abstract

This document mainly focuses on the problems existed in floating experiment such as software complexity, real-time difficulty and test method lackness. According to the simulation requirment, experiment of flotation units is proposed, hardware system of the simulation system is designed and software system is designed using virtual instrument technology. A variety of attitude maneuver modes are designed for the attitude control and simulation of multi-rigid-body physical prototype spacecraft. Experimental results indicate that the experimental system based on flotation units meets the requirements of multi-rigid-body spacecraft attitude control and simulation, and technology employed effectively solves the problems in the experiment.

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  - Yong-ming Gao
AU  - Zhao-ming Li
PY  - 2015/12
DA  - 2015/12
TI  - Physical Simulation Experiment System of Multi-Rigid-Body Spacecraft Attitude Control Based on Micro-Gravity Floating Platform Environment
BT  - Proceedings of the 2015 Joint International Mechanical, Electronic and Information Technology Conference
PB  - Atlantis Press
SP  - 1047
EP  - 1053
SN  - 2352-538X
UR  - https://doi.org/10.2991/jimet-15.2015.197
DO  - 10.2991/jimet-15.2015.197
ID  - Gao2015/12
ER  -