在研究起重机吊重系统防摇控制时,可以分别对小车位移和摆角子系统进行控制器设计。由于在起重机摆角子系统中吊重摆角角速度一般靠传感器进行测量,增加了运行和维护成本。为此提出了设计起重机摆角子系统非线性扩张状态观测器对起重机...在研究起重机吊重系统防摇控制时,可以分别对小车位移和摆角子系统进行控制器设计。由于在起重机摆角子系统中吊重摆角角速度一般靠传感器进行测量,增加了运行和维护成本。为此提出了设计起重机摆角子系统非线性扩张状态观测器对起重机摆角子系统状态信息进行重构,软测量摆角角速度。给出了观测器的结构方程,并运用Matlab对观测器参数进行了优化整定。参数整定后的扩张状态观测器能够在0.3 s内估计出系统摆角和摆角速度,并且在0.5 s内估计出了系统的外界干扰。仿真结果表明:经过Matlab参数整定的扩张状态观测器(extend state observer,ESO)可以实现对非线性的起重机摆角子系统状态信息的软测量。展开更多
In this paper, the attitude control problem of rigid body is addressed with considering inertia uncertainty,bounded time-varying disturbances, angular velocity-free measurement, and unknown non-symmetric saturation in...In this paper, the attitude control problem of rigid body is addressed with considering inertia uncertainty,bounded time-varying disturbances, angular velocity-free measurement, and unknown non-symmetric saturation input. Using a mathematical transformation, the effects of bounded time-varying disturbances, uncertain inertia,and saturation input are combined as total disturbances. A novel finite-time observer is designed to estimate the unknown angular velocity and the total disturbances. For attitude control, an observer-based sliding-mode control protocol is proposed to force the system state convergence to the desired sliding-mode surface; the finite-time stability is guaranteed via Lyapunov theory analysis. Finally, a numerical simulation is presented to illustrate the effective performance of the proposed sliding-mode control protocol.展开更多
文摘在研究起重机吊重系统防摇控制时,可以分别对小车位移和摆角子系统进行控制器设计。由于在起重机摆角子系统中吊重摆角角速度一般靠传感器进行测量,增加了运行和维护成本。为此提出了设计起重机摆角子系统非线性扩张状态观测器对起重机摆角子系统状态信息进行重构,软测量摆角角速度。给出了观测器的结构方程,并运用Matlab对观测器参数进行了优化整定。参数整定后的扩张状态观测器能够在0.3 s内估计出系统摆角和摆角速度,并且在0.5 s内估计出了系统的外界干扰。仿真结果表明:经过Matlab参数整定的扩张状态观测器(extend state observer,ESO)可以实现对非线性的起重机摆角子系统状态信息的软测量。
基金supported by the National Natural Science Foundation of China (No. 61403399)
文摘In this paper, the attitude control problem of rigid body is addressed with considering inertia uncertainty,bounded time-varying disturbances, angular velocity-free measurement, and unknown non-symmetric saturation input. Using a mathematical transformation, the effects of bounded time-varying disturbances, uncertain inertia,and saturation input are combined as total disturbances. A novel finite-time observer is designed to estimate the unknown angular velocity and the total disturbances. For attitude control, an observer-based sliding-mode control protocol is proposed to force the system state convergence to the desired sliding-mode surface; the finite-time stability is guaranteed via Lyapunov theory analysis. Finally, a numerical simulation is presented to illustrate the effective performance of the proposed sliding-mode control protocol.
