机译:火星进入轨迹跟踪的有限时间超扭曲滑模控制
Southeast Univ, Sch Automat, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China;
Southeast Univ, Sch Automat, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China;
Southeast Univ, Sch Automat, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China;
Southeast Univ, Sch Automat, Key Lab Measurement & Control Complex Syst Engn, Minist Educ, Nanjing 210096, Jiangsu, Peoples R China;
Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China|Inst Instrument Sci & Optoelect Engn, Beijing 100191, Peoples R China;
机译:具有有限时间收敛的火星条目轨迹跟踪的自适应滑模控制
机译:基于障碍Lyapunov功能基于MARS大气入口轨迹跟踪的滑动模式控制,输入饱和度约束
机译:通过扩展的超扭曲观测器对主动悬架系统进行有限时间的滑模跟踪控制
机译:基于高阶滑模控制的火星大气进入轨迹跟踪
机译:使用滑动窗口估计器和自主车辆轨迹跟踪控制的实时,分米精度导航。
机译:用于欠驱动系统的平滑超扭曲滑模控制
机译:使用改进的超扭转二阶滑动模式的三转子UAV有限时间高度和姿态跟踪