A fault tolerant control （FTC） design technique against actuator stuck faults is investigated using integral-type sliding mode control （ISMC） with application to spacecraft attitude maneuvering control system. The...A fault tolerant control （FTC） design technique against actuator stuck faults is investigated using integral-type sliding mode control （ISMC） with application to spacecraft attitude maneuvering control system. The principle of the proposed FTC scheme is to design an integral-type sliding mode attitude controller using on-line parameter adaptive updating law to compensate for the effects of stuck actuators. This adaptive law also provides both the estimates of the system parameters and external disturbances such that a prior knowledge of the spacecraft inertia or boundedness of disturbances is not required. Moreover, by including the integral feedback term, the designed controller can not only tolerate actuator stuck faults, but also compensate the disturbances with constant components. For the synthesis of controller, the fault time, patterns and values are unknown in advance, as motivated from a practical spacecraft control application. Complete stability and performance analysis are presented and illustrative simulation results of application to a spacecraft show that high precise attitude control with zero steady-error is successfully achieved using various scenarios of stuck failures in actuators.展开更多
为了发掘X舵潜艇在持续高强度随机干扰环境下稳定操纵的能力,建立了某型X舵潜艇六自由度运动模型,分析了X舵的操纵规律,在X舵模糊控制主体、智能模糊积分环节及控制权限动态分配三个方面对X舵模糊控制系统进行了设计.仿真计算表明:模糊...为了发掘X舵潜艇在持续高强度随机干扰环境下稳定操纵的能力,建立了某型X舵潜艇六自由度运动模型,分析了X舵的操纵规律,在X舵模糊控制主体、智能模糊积分环节及控制权限动态分配三个方面对X舵模糊控制系统进行了设计.仿真计算表明:模糊控制系统在潜艇低频和高频随机干扰力和力矩峰值分别为500 k N和400k N·m的作用下,基本能将深度和姿态稳定在期望值,控制效果明显好于比例积分微分(PID)控制器,但在高频干扰下存在小范围抖振现象.采用变论域思想对模糊控制系统进行改进,对深度、纵倾、横倾和航向的误差变化率采用论域在线调节机制,在同样的干扰环境下能够消除深度和姿态的抖振,实现对潜艇复杂条件下航行的精准稳定控制.展开更多
基金National Natural Science Foundation of China(61004072)Fundamental Research Funds for the Central Universities(HIT.NSRIF.2009003)+1 种基金Research Fund for the Doctoral Program of Higher Education of China (20070213061, 20102302110031)Scientific Research Foundation for the Returned Overseas Chinese Scholars of Harbin (2010RFLXG001)
文摘A fault tolerant control （FTC） design technique against actuator stuck faults is investigated using integral-type sliding mode control （ISMC） with application to spacecraft attitude maneuvering control system. The principle of the proposed FTC scheme is to design an integral-type sliding mode attitude controller using on-line parameter adaptive updating law to compensate for the effects of stuck actuators. This adaptive law also provides both the estimates of the system parameters and external disturbances such that a prior knowledge of the spacecraft inertia or boundedness of disturbances is not required. Moreover, by including the integral feedback term, the designed controller can not only tolerate actuator stuck faults, but also compensate the disturbances with constant components. For the synthesis of controller, the fault time, patterns and values are unknown in advance, as motivated from a practical spacecraft control application. Complete stability and performance analysis are presented and illustrative simulation results of application to a spacecraft show that high precise attitude control with zero steady-error is successfully achieved using various scenarios of stuck failures in actuators.
文摘为了发掘X舵潜艇在持续高强度随机干扰环境下稳定操纵的能力,建立了某型X舵潜艇六自由度运动模型,分析了X舵的操纵规律,在X舵模糊控制主体、智能模糊积分环节及控制权限动态分配三个方面对X舵模糊控制系统进行了设计.仿真计算表明:模糊控制系统在潜艇低频和高频随机干扰力和力矩峰值分别为500 k N和400k N·m的作用下,基本能将深度和姿态稳定在期望值,控制效果明显好于比例积分微分(PID)控制器,但在高频干扰下存在小范围抖振现象.采用变论域思想对模糊控制系统进行改进,对深度、纵倾、横倾和航向的误差变化率采用论域在线调节机制,在同样的干扰环境下能够消除深度和姿态的抖振,实现对潜艇复杂条件下航行的精准稳定控制.
