DocumentCode
3410118
Title
Application of H∞ Control Based on Mixed Sensitivity in the Electro-hydraulic Load Simulator
Author
Wang, Jingfu ; Liang, Lihua ; Zhang, Songtao ; Ye, Zhengmao ; Li, Hongren
Author_Institution
Harbin Eng. Univ., Harbin
fYear
2007
fDate
5-8 Aug. 2007
Firstpage
2991
Lastpage
2996
Abstract
The electro-hydraulic load simulator is an essential rig for the performance and stability test of aircraft rudder system. Its function is to reproduce, under laboratory conditions, the aerodynamic load of the rudder system. The model of electro-hydraulic load simulator is developed and the affecting factors of extraneous force are determined. To replicate the wide spectrum of aerodynamic load when the load spring stiffness varies within a definite bound, a loading controller is designed with H∞ mixed sensitivity approach. It´s solved by the linear matrix inequality algorithm through selecting the suitable weighted functions. It´s testified by experiments that the proposed controller can satisfy robust stability and robust performance when the load spring stiffness varies. It also can eliminate extraneous force and improve the passive loading performance with the compensation networks based on the structure invariance principle.
Keywords
Hinfin control; aerospace control; aircraft; compensation; electrohydraulic control equipment; force control; hydraulic systems; linear matrix inequalities; robust control; sensitivity analysis; springs (mechanical); Hinfin control; aerodynamic load; aircraft rudder system; compensation network; electrohydraulic load simulator; extraneous force; linear matrix inequality; load spring stiffness; loading controller; mixed sensitivity; robust stability; Aerodynamics; Aircraft; Automation; Force control; Mechatronics; Robust control; Springs; Stability; System testing; Uncertainty; H∞ control; electro-hydraulic load simulator; extraneous force; mixed sensitivity;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2007. ICMA 2007. International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-0827-6
Electronic_ISBN
978-1-4244-0828-3
Type
conf
DOI
10.1109/ICMA.2007.4304036
Filename
4304036
Link To Document