期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
Autotuning algorithm of particle swarm PID parameter based on D-Tent chaotic model 被引量:7
1
作者 Min Zhu Chunling Yang Weiliang Li 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2013年第5期828-837,共10页
An improved particle swarm algorithm based on the D-Tent chaotic model is put forward aiming at the standard particle swarm algorithm. The convergence rate of the late of proposed algorithm is improved by revising the... An improved particle swarm algorithm based on the D-Tent chaotic model is put forward aiming at the standard particle swarm algorithm. The convergence rate of the late of proposed algorithm is improved by revising the inertia weight of global optimal particles and the introduction of D-Tent chaotic sequence. Through the test of typical function and the autotuning test of proportionalintegral-derivative (PID) parameter, finally a simulation is made to the servo control system of a permanent magnet synchronous motor (PMSM) under double-loop control of rotating speed and current by utilizing the chaotic particle swarm algorithm. Studies show that the proposed algorithm can reduce the iterative times and improve the convergence rate under the condition that the global optimal solution can be got. 展开更多
关键词 D-Tent particle swarm proportional-integral- derivative pid parameter optimization.
下载PDF
Survey on nonlinear reconfigurable flight control 被引量:2
2
作者 Xunhong Lv Bin Jiang +1 位作者 Ruiyun Qi Jing Zhao 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2013年第6期971-983,共13页
An overview on nonlinear reconfigurable flight control approaches that have been demonstrated in flight-test or highfidelity simulation is presented. Various approaches for reconfigurable flight control systems are co... An overview on nonlinear reconfigurable flight control approaches that have been demonstrated in flight-test or highfidelity simulation is presented. Various approaches for reconfigurable flight control systems are considered, including nonlinear dynamic inversion, parameter identification and neural network technologies, backstepping and model predictive control approaches. The recent research work, flight tests, and potential strength and weakness of each approach are discussed objectively in order to give readers and researchers some reference. Finally, possible future directions and open problems in this area are addressed. 展开更多
关键词 reconfigurable flight control (RFC) nonlinear dynamic inversion (NDI) BACKSTEPPING neural network (NN) model predictive control (MPC) parameter identification pid adaptive control flight control.
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部