Dynamic Integral Sliding Mode for Launch Vehicle Attitude Control System
As it is known that launch vehicle is facing a very harsh environment during the fight process. The challenge of various perturbations and uncertainties has lead to many traditional control methods’ failure to meet the requirements of attitude control system. Due to the main advantage of sliding mode control’s robustness to the system uncertainties and disturbances in the so-called sliding mode, it has been widely used in engineering. In this paper, regarding particularly on chattering problem, the authors developed a novel dynamic integral sliding mode control scheme and the comparative simulation results carried out with traditional dynamic integral sliding mode demonstrates the superiority of the newly designed control law.
Launch vehicle Attitude control Dynamic integral sliding mode control.
王子瑞 刘磊 王永骥 王志燊
图像信息处理与智能控制教育部重点实验室，控制科学与工程系，华中科技大学 武汉 430074
国际会议
The 24th Chinese Control and Decision Conference (第24届中国控制与决策学术年会 2012 CCDC)
太原
英文
1725-1730
2012-05-23（万方平台首次上网日期，不代表论文的发表时间）