提出一种dq坐标系下静止无功发生器的自抗扰解耦控制方法。首先针对静止无功发生器(static var generator,SVG)非线性、强耦合的特点,建立并设计基于自抗扰技术的多变量解耦控制系统。其次,为克服一般控制算法难以解决的高频振荡和滤波...提出一种dq坐标系下静止无功发生器的自抗扰解耦控制方法。首先针对静止无功发生器(static var generator,SVG)非线性、强耦合的特点,建立并设计基于自抗扰技术的多变量解耦控制系统。其次,为克服一般控制算法难以解决的高频振荡和滤波效果差的问题,设计最速控制综合函数作为跟踪微分器。另外设计自抗扰线性和非线性两种控制器,并与PI控制算法进行比较,通过Matlab仿真和样机实验,验证了所设计的基于非线性自抗扰技术的多变量解耦控制算法可实现SVG输出电流在dq轴下的解耦,使系统具有较快的动态响应和较强的鲁棒性及抗干扰性,尤其具有单参数调节和无超调的优良性能。展开更多
A novel robust fault tolerant controller is developed for the problem of attitude control of a quadrotor aircraft in the presence of actuator faults and wind gusts in this paper.Firstly, a dynamical system of the quad...A novel robust fault tolerant controller is developed for the problem of attitude control of a quadrotor aircraft in the presence of actuator faults and wind gusts in this paper.Firstly, a dynamical system of the quadrotor taking into account aerodynamical effects induced by lateral wind and actuator faults is considered using the Newton-Euler approach. Then,based on active disturbance rejection control(ADRC), the fault tolerant controller is proposed to recover faulty system and reject perturbations. The developed controller takes wind gusts,actuator faults and measurement noises as total perturbations which are estimated by improved extended state observer(ESO)and compensated by nonlinear feedback control law. So, the developed robust fault tolerant controller can successfully accomplish the tracking of the desired output values. Finally, some simulation studies are given to illustrate the effectiveness of fault recovery of the proposed scheme and also its ability to attenuate external disturbances that are introduced from environmental causes such as wind gusts and measurement noises.展开更多
文摘提出一种dq坐标系下静止无功发生器的自抗扰解耦控制方法。首先针对静止无功发生器(static var generator,SVG)非线性、强耦合的特点,建立并设计基于自抗扰技术的多变量解耦控制系统。其次,为克服一般控制算法难以解决的高频振荡和滤波效果差的问题,设计最速控制综合函数作为跟踪微分器。另外设计自抗扰线性和非线性两种控制器,并与PI控制算法进行比较,通过Matlab仿真和样机实验,验证了所设计的基于非线性自抗扰技术的多变量解耦控制算法可实现SVG输出电流在dq轴下的解耦,使系统具有较快的动态响应和较强的鲁棒性及抗干扰性,尤其具有单参数调节和无超调的优良性能。
基金supported by the National Natural Science Foundation of China(61573282)the Foundation of the Education Department of Sichuan Province(16ZA0132)the Foundation of Robot Technology Used for Special Environment,Key Laboratory of Sichuan Province(13zxtk06)
文摘A novel robust fault tolerant controller is developed for the problem of attitude control of a quadrotor aircraft in the presence of actuator faults and wind gusts in this paper.Firstly, a dynamical system of the quadrotor taking into account aerodynamical effects induced by lateral wind and actuator faults is considered using the Newton-Euler approach. Then,based on active disturbance rejection control(ADRC), the fault tolerant controller is proposed to recover faulty system and reject perturbations. The developed controller takes wind gusts,actuator faults and measurement noises as total perturbations which are estimated by improved extended state observer(ESO)and compensated by nonlinear feedback control law. So, the developed robust fault tolerant controller can successfully accomplish the tracking of the desired output values. Finally, some simulation studies are given to illustrate the effectiveness of fault recovery of the proposed scheme and also its ability to attenuate external disturbances that are introduced from environmental causes such as wind gusts and measurement noises.