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    题名 作者 年代 出处 被引量
1Disturbance observer based time-varying sliding mode control for uncertain mechanical system显示文摘It is now well known that the time-varying sliding mode control (TVSMC) is characterized by its global robustness against matched model uncertainties and disturbances. The accurate tracking problem of the mechanical system in the presence of the parametric uncertainty and external disturbance is addressed in the TVSMC framework. Firstly, an exponential TVSMC algorithm is designed and the main features are analyzed. Especially, the control parameter is obtained by solving an optimal problem. Subsequently, the global chattering problem in TVSMC is considered. To reduce the static error resulting from the continuous TVSMC algorithm, a disturbance observer based time-varying sliding mode control (DOTVSMC) algorithm is presented. The detailed design principle and the stability of the closed-loop system under the composite controller are provided. Simulation results verify the effectiveness of the proposed algorithm.Binglong Cong Xiangdong Liu Zhen Chen 2012Journal of Systems Engineering and Electronics2012,23,1:12
2A Precise and Robust Control Strategy for Rigid Spacecraft Eigenaxis Rotation显示文摘Eigenaxis 旋转通常由于它在二取向之间的最短的尖路径的体质为快速的态度演习被认为是近最小的时间策略。在这份报纸,僵硬太空船 eigenaxis 旋转的柔韧的控制问题经由变化时间的滑动模式控制(TVSMC ) 被调查技术。外部骚乱和参数变化被考虑。这柔韧的 eigenaxis 旋转策略的主要特征被一个 TVSMC 算法首先表明。全球滑动阶段象靠近环的系统稳定性一样被证明。另外,为 eigenaxis 旋转的必要条件被提供。随后,压制全球啁啾并且改进控制精确性,骚乱基于观察员的变化时间的滑动模式控制(DOTVSMC ) 算法被介绍,在边界层途径被用来弄软啁啾和骚乱的地方,观察员被设计稀释不希望得到的效果。太空船态度被修改 Rodrigues 参数(MRP ) 为非冗余性代表。最后,数字模拟被采用说明建议策略的有效性,在脉搏宽度脉搏频率(PWPF ) 技术被利用调制开关推进器的地方。CONG Binglong LIU Xiangdong CHEN Zhen 2011Chinese Journal of Aeronautics2011,24,4:2
3Switching Gain Reduc- tion in Adaptive Sliding Mode Control for Rigid Spacecraft Attitude Maneuvers 显示文摘Zhen Chen Binglong cong Xiangdong Liu 2013Mathematical Problems in Engineering2013,2013,:1
4Distributed attitude synchronization of formation flying via consensus-based virtual structure 显示文摘Cong Binglong Liu Xiangdong Chen Zhen 2011Acta Astronautica2011,68,1112:1
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