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机译:具有多个执行器故障和饱和度的刚性航天器的集成故障估计和容错姿态控制
Nanjing Univ Posts & Telecommun Coll Automat Nanjing 210046 Peoples R China;
Tongji Univ Coll Elect & Informat Engn Shanghai 200092 Peoples R China;
variable structure systems; observers; fault tolerance; space vehicles; control system synthesis; actuators; Lyapunov methods; closed loop systems; stability; attitude control; finite-time fault-tolerant attitude tracking controller; closed-loop attitude system; good fault-tolerant performance; considering actuator saturation; control approach; fault tolerant attitude control; integrated fault estimation; fault-tolerant control design; rigid spacecraft attitude system; inertia uncertainties; input saturation; different type multiple actuator faults; sliding mode FE observer; nonsingular fast terminal sliding mode control technology; finite-time fault-tolerant attitude stabilisation controller;
机译:具有多个执行器故障的刚性航天器姿态系统的集成故障估计和容错控制
机译:基于观察者的刚性航天器具有致动器饱和度和故障的容错姿态跟踪控制
机译:具有执行器饱和和故障的航天器姿态操纵的主动容错控制系统设计
机译:具有执行器故障和执行器饱和度的UAV姿态控制系统有限时间容错控制设计
机译:在已知和未知故障下,过度驱动的自动驾驶汽车的遗传多模型容错控制。
机译:具有传感器和执行器故障的无人机滑模容错控制
机译:基于复合控制的静电航天器静态航天器态度跟踪