ATTITUDE STABILIZATION OF AN UNDER-ACTUATED RIGID SPACECRAFT VIA LOGIC-BASED SWITCHING CONTROL

摘要：

The attitude stabilization control for an under-actuated spacecraft with two moving mass is considered in this paper. The kinematic and dynamic equations of the spacecraft are derived. A hybrid controller is proposed to yield global convergence to an arbitrarily small neighborhood of the origin. Simulation results show the superiority of the new type configuration scheme for moving mass moment control spacecraft.

关键词： Attitude stabilization Under-actuated spacecraft Hybrid feedback control

作者: FENG-HUA HE KE-MAO MA YU YAO

作者单位: Control and Simulation Center, Harbin Institute of Technology, Harbin 150080, China

会议类型: 国际会议

会议名称: 2008 International Conference on Machine Learning and Cybernetics(2008机器学习与控制论国际会议)

会议地点: 昆明

会议语种:英文

页码: 1914-1919

在线出版日期: 2008-07-12（万方平台首次上网日期，不代表论文的发表时间）