针对传统PI应用于静止无功补偿器(static var compen-sator,SVC)这个非线性复杂系统上,所体现出的快速性与稳定性之间的矛盾,以及对精确数学模型的依赖性,适应性及鲁棒性较差,该文设计了以非线性函数与传统PI控制器串联起来构成非线性P...针对传统PI应用于静止无功补偿器(static var compen-sator,SVC)这个非线性复杂系统上,所体现出的快速性与稳定性之间的矛盾,以及对精确数学模型的依赖性,适应性及鲁棒性较差,该文设计了以非线性函数与传统PI控制器串联起来构成非线性PI控制器,简单易于实现。并且提出基于改进的单纯形加速算法(simplex method,SPX),以时间乘以误差绝对值积分(integrate of time multiplied absolute error,ITAE)准则作为寻优目标函数,对非线性PI控制器的参数KP、KI进行实时调整、寻优,使SVC系统的瞬态响应过程达到最佳。仿真和实际应用结果表明该最优非线性PI控制器,不但能快速、无超调的跟踪SVC系统的电压设定值,而且可实现对无功功率、三相不平衡等多个因素的综合补偿,具有较强的鲁棒性、适应性和较高的补偿精度。展开更多
Taking the accelerometer installation errors into consideration, the attitude optimization algorithm of Gyro Free Inertial Meastement Unit （GFIMU） is studied in the high spinning condition in this paper. A ten-accel...Taking the accelerometer installation errors into consideration, the attitude optimization algorithm of Gyro Free Inertial Meastement Unit （GFIMU） is studied in the high spinning condition in this paper. A ten-accelerometer configuration is designed so as to establish a mathematical model to acquire the angular speeds in the case of installation errors. Precision of the algorithm is evaluated by using damping GaussNewton method. A large amotmt of sinmlation results show that ff the accelertlmter＇s angleinstallation errors main-tain small （〈5°）, the errors of attitude angles can be limited within ±1°. Hence, the algorithm has a great applicable value in engineering.展开更多
文摘针对传统PI应用于静止无功补偿器(static var compen-sator,SVC)这个非线性复杂系统上,所体现出的快速性与稳定性之间的矛盾,以及对精确数学模型的依赖性,适应性及鲁棒性较差,该文设计了以非线性函数与传统PI控制器串联起来构成非线性PI控制器,简单易于实现。并且提出基于改进的单纯形加速算法(simplex method,SPX),以时间乘以误差绝对值积分(integrate of time multiplied absolute error,ITAE)准则作为寻优目标函数,对非线性PI控制器的参数KP、KI进行实时调整、寻优,使SVC系统的瞬态响应过程达到最佳。仿真和实际应用结果表明该最优非线性PI控制器,不但能快速、无超调的跟踪SVC系统的电压设定值,而且可实现对无功功率、三相不平衡等多个因素的综合补偿,具有较强的鲁棒性、适应性和较高的补偿精度。
基金supported by National Key Laboratory for Electronic Measurement and Technology(No.9140C120401080C12)
文摘Taking the accelerometer installation errors into consideration, the attitude optimization algorithm of Gyro Free Inertial Meastement Unit （GFIMU） is studied in the high spinning condition in this paper. A ten-accelerometer configuration is designed so as to establish a mathematical model to acquire the angular speeds in the case of installation errors. Precision of the algorithm is evaluated by using damping GaussNewton method. A large amotmt of sinmlation results show that ff the accelertlmter＇s angleinstallation errors main-tain small （〈5°）, the errors of attitude angles can be limited within ±1°. Hence, the algorithm has a great applicable value in engineering.
