Title :
Robust controller design and experiment for electric load simulator
Author :
Huang, Yong ; Chen, Kang ; Wei, Jianli
Author_Institution :
Sch. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
Abstract :
According to the operating principle of the electric load simulator, the mathematic model of its actuating mechanism is built. Then, combining with the load gradient, the H-infinity controller based on the mixed sensitivity method is designed and synthesized by selecting the appropriate joint stiffness and weight functions. Last, the simulation and experiment results show that the controller can not only make the steady-state error of the closed loop system less than 0.5%, but also make the error of amplitude less than 10% and the lag of phase less than 10 degree when the system is stimulated by 10Hz sine signal.
Keywords :
H∞ control; aerospace simulation; aircraft control; closed loop systems; control system synthesis; load (electric); robust control; H-infinity controller; actuating mechanism; aircraft; closed loop system; electric load simulator; load gradient; mathematic model; mixed sensitivity method; robust controller design; steady-state error; stiffness function; weight function; Atmospheric modeling; Petroleum; Shafts; H-inf control; electric load simulator; mixed sensitivity;
Conference_Titel :
Advanced Computer Theory and Engineering (ICACTE), 2010 3rd International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6539-2
DOI :
10.1109/ICACTE.2010.5579642