Physical Simulation Experiment System of Multi-Rigid-Body Spacecraft Attitude Control Based on Micro-Gravity Floating Platform Environment
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.
multi-rigid-body spacecraft flotation units real-time simulation virtual instrument
Yong-ming Gao Zhao-ming Li
The Academy of Equipment
国际会议
重庆
英文
1047-1053
2015-12-18（万方平台首次上网日期，不代表论文的发表时间）