信阳师范学院学报(自然科学版)2008,Vol.21Issue(1):21-23,3.
带柔性附件的充液飞行器姿态动力学与控制
Attitude Dynamics and Control of Spacecraft Filled with Liquid and Attached with a Flexible Appendage
摘要
Abstract
The attitude dynamics,stability and control of the spacecraft system coupled with fluid,rigid and elastic bodies are studied in this paper. The control laws are given respectively for every part of the system. It is proved that the control laws might lead the attitude of the system to the desired position and that the controlled system is exponentially asymptotically stable.关键词
耦合系统/动力学/控制/稳定性Key words
coupled system/dynamics/control/stability分类
数理科学引用本文复制引用
徐建国..带柔性附件的充液飞行器姿态动力学与控制[J].信阳师范学院学报(自然科学版),2008,21(1):21-23,3.基金项目
The National Natural Science Foundation of China (10572156) (10572156)
The Natural Science Foundation of Henan province (072300410270) (072300410270)