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基于目标全息反馈的STATCOM与发电机励磁的多目标非线性协调控制 被引量:7
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作者 李啸骢 谢醉冰 +1 位作者 肖明 赵亚楠 《电力系统保护与控制》 EI CSCD 北大核心 2013年第17期109-115,共7页
针对以往静止同步补偿器(STATCOM)数学模型具有较多约束条件的问题,以STATCOM内部并联电容的直流电压Udc为切入点,采用STATCOM的脉冲控制角和STATCOM超前系统电压角为控制量,提出一种新型的STATCOM数学模型。借助非线性多目标控制设计理... 针对以往静止同步补偿器(STATCOM)数学模型具有较多约束条件的问题,以STATCOM内部并联电容的直流电压Udc为切入点,采用STATCOM的脉冲控制角和STATCOM超前系统电压角为控制量,提出一种新型的STATCOM数学模型。借助非线性多目标控制设计理念,选取6个跟踪状态目标;基于目标全息反馈控制原理,将非线性系统的多目标控制问题转换到线性系统中,得到包含全部控制目标反馈信息的非线性控制律u,完成了凸极式发电机励磁与STATCOM协调控制策略的设计,并通过单机无穷大系统对其进行暂态仿真。仿真结果表明:利用目标全息反馈非线性控制设计方法设计的协调控制律能较好地改善发电机的输出特性,有效地抑制系统电压的静态偏移,改善电力系统的暂态稳定性,提升系统协调控制的动、静态性能。 展开更多
关键词 STATCOM 发电机励磁 目标全息反馈 非线性多目标控制 协调控制
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基于terminal滑模与控制分配的飞翼布局无人机姿态控制 被引量:3
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作者 谭健 周洲 +1 位作者 祝小平 徐明兴 《西北工业大学学报》 EI CAS CSCD 北大核心 2014年第4期505-510,共6页
对于风场扰动中的飞翼布局无人机,需要考虑模型参数不确定和外界干扰对姿态控制的影响,以及解决操纵面冗余、附加力效应显著、多轴操纵耦合、舵效非线性等特殊问题。采用基于扩张状态观测器的terminal滑模和多目标非线性控制分配对姿态... 对于风场扰动中的飞翼布局无人机,需要考虑模型参数不确定和外界干扰对姿态控制的影响,以及解决操纵面冗余、附加力效应显著、多轴操纵耦合、舵效非线性等特殊问题。采用基于扩张状态观测器的terminal滑模和多目标非线性控制分配对姿态角的跟踪控制问题进行了研究,将扩张状态观测器与基于饱和函数的terminal滑模控制器相结合,在名义滑模控制律的基础上采用扩张状态观测器实现对干扰的估计和补偿,有效提高了系统的鲁棒性和控制精度,并且充分利用冗余操纵面,根据飞行任务需求,实现对多种目标综合权衡的非线性控制分配。 展开更多
关键词 飞翼布局无人机 风场扰动 扩张状态观测器 TERMINAL滑模控制 多目标非线性控制分配
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Optimal design of dynamic and control performance for planar manipulator 被引量:6
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作者 YOU Wei KONG Min-xiu +1 位作者 SUN Li-ning DU Zhi-jiang 《Journal of Central South University》 SCIE EI CAS 2012年第1期108-116,共9页
A design and optimization approach of dynamic and control performance for a two-DOF planar manipulator was proposed.After the kinematic and dynamic analysis,several advantages of the mechanism were illustrated,which m... A design and optimization approach of dynamic and control performance for a two-DOF planar manipulator was proposed.After the kinematic and dynamic analysis,several advantages of the mechanism were illustrated,which made it possible to obtain good dynamic and control performances just through mechanism optimization.Based on the idea of design for control(DFC),a novel kind of multi-objective optimization model was proposed.There were three optimization objectives:the index of inertia,the index describing the dynamic coupling effects and the global condition number.Other indexes to characterize the designing requirements such as the velocity of end-effector,the workspace size,and the first mode natural frequency were regarded as the constraints.The cross-section area and length of the linkages were chosen as the design variables.NSGA-II algorithm was introduced to solve this complex multi-objective optimization problem.Additional criteria from engineering experience were incorporated into the selecting of final parameters among the obtained Pareto solution sets.Finally,experiments were performed to validate the linear dynamic structure and control performances of the optimized mechanisms.A new expression for measuring the dynamic coupling degree with clear physical meaning was proposed.The results show that the optimized mechanism has an approximate decoupled dynamics structure,and each active joint can be regarded as a linear SISO system.The control performances of the linear and nonlinear controllers were also compared.It can be concluded that the optimized mechanism can achieve good control performance only using a linear controller. 展开更多
关键词 mechanism optimization dynamic optimization design for control multi-objective optimization
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