机译:基于有限时间干扰观测器的整体滑模控制,用于执行器故障时的姿态稳定
Shanghai Maritime Univ, Inst Logist Sci & Engn, Shanghai 201306, Peoples R China;
Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China;
Shanghai Maritime Univ, Inst Logist Sci & Engn, Shanghai 201306, Peoples R China;
Shanghai Maritime Univ, Inst Logist Sci & Engn, Shanghai 201306, Peoples R China|Instituto Telecomunicacoes, P-1049001 Lisbon, Portugal;
space vehicles; Lyapunov methods; stability; observers; attitude control; aircraft control; variable structure systems; control system synthesis; closed loop systems; actuators; integral sliding mode control; actuator failure; fault tolerant attitude control scheme; external disturbance torques; simple finite-time disturbance observer; synthetic uncertainty; closed-loop attitude control system; finite-time stability; attitude control approach; integral sliding mode-based finite-time fault tolerant attitude stabilisation controller;
机译:基于非线性扰动观测器的多扰动多种扰动的多种子体系统分布式有限时间整体滑模控制
机译:基于有限时间非线性扰动观测器的PMSM驱动器离散积分滑模控制
机译:基于复合观测器的非线性系统的整体滑动模式动态跟踪控制,执行器故障和错配干扰
机译:执行器故障下基于有限时间扰动观测器的姿态稳定控制
机译:基于自适应观测器和滑模观测器的民用飞机执行器故障诊断。
机译:基于分散滑模观测器的双闭环容错控制用于可重构机械手以防止执行器故障
机译:执行器卡滞故障下航天器姿态操纵的自适应积分型滑模控制
机译:利用基于扰动观测器的转矩控制改进串联弹性作动器的阻抗渲染。