PIM-based Controller Design for Systems with Network-Induced Time Delays

Author(s):  
Suhaila Badarol Hisham ◽  
Noriyuki Hori

2020 ◽  
Vol 385 ◽  
pp. 292-299 ◽  
Author(s):  
Chenglong Wang ◽  
Haiyang Fang ◽  
Shuping He


2012 ◽  
Vol 31 (5) ◽  
pp. 1653-1676 ◽  
Author(s):  
Hsun-Pang Wang ◽  
Xiaohui Gu ◽  
Linbo Xie ◽  
Leang-San Shieh ◽  
Jason S. H. Tsai ◽  
...  




Volume 1 ◽  
2004 ◽  
Author(s):  
Clarice Wagner-Nachshoni ◽  
Yoram Halevi

A method of noncollocated controller design for non-uniform flexible structures, governed by the wave equation, is proposed. An exact, infinite dimensional, transfer function, relating the actuation and measurement points, with general boundary conditions, is derived for the multi-link case. Three modeling methods are presented and discussed. A key element of the model is the existence of time delays, due to the wave motion, which play a major role in the controller design. The design consists of two stages. First an inner rate loop is closed in order to improve the system dynamic behavior. It leads to a finite dimensional plus delay inner closed loop, which is the equivalent plant for the outer loop. In the second stage an outer noncollocated position loop is closed. It has the structure of an observer–predictor control scheme to compensate for the response delay. The resulting overall transfer function is second order, with arbitrarily assigned dynamics, plus delay.



10.5772/10583 ◽  
2008 ◽  
Vol 5 (4) ◽  
pp. 34 ◽  
Author(s):  
Jianfu Du ◽  
Konstantin Kondak ◽  
Markus Bernard ◽  
Yaou Zhang ◽  
Tiansheng Lü ◽  
...  

Kinematical and dynamical equations of a small scale unmanned helicoper are presented in the paper. Based on these equations a model predictive control (MPC) method is proposed for controlling the helicopter. This novel method allows the direct accounting for the existing time delays which are used to model the dynamics of actuators and aerodynamics of the main rotor. Also the limits of the actuators are taken into the considerations during the controller design. The proposed control algorithm was verified in real flight experiments where good perfomance was shown in postion control mode.



2005 ◽  
Vol 44 (6) ◽  
pp. 1832-1841 ◽  
Author(s):  
Tao Liu ◽  
Weidong Zhang ◽  
Danying Gu


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