DocumentCode
164197
Title
Linear Parameter Varying control synthesis: State feedback versus H∞ technique with application to quadrotor UA V
Author
Sadeghzadeh, Iman ; Chamseddine, Abbas ; Theilliol, Didier ; Youmin Zhang
Author_Institution
Dept. of Mech. & Ind. Eng., Concordia Univ., Montreal, QC, Canada
fYear
2014
fDate
27-30 May 2014
Firstpage
1099
Lastpage
1104
Abstract
This paper focuses on the synthesis of Linear Parameter Varying (LPV) control based on two different LPV control structures. In the first structure the H∞ self-Gain-Scheduling (GS) control technique is used to obtain the LPV controller and in the second method, the composite quadratic Lyapunov function and the quadratic cost function are used to find the optimal state feedback gain. Finally, a six-degree of freedom quadrotor helicopter is used as an illustrative plant to compare the results of both LPV control structures.
Keywords
H∞ control; Lyapunov methods; autonomous aerial vehicles; control system synthesis; helicopters; linear systems; mobile robots; state feedback; H∞ self-gain-scheduling control technique; H∞ technique; LPV control synthesis; linear parameter varying control synthesis; optimal state feedback gain; quadratic Lyapunov function; quadratic cost function; quadrotor UAV; six-degree of freedom quadrotor helicopter; Brushless motors; Educational institutions; Helicopters; Lyapunov methods; Propellers; Rotors; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2014 International Conference on
Conference_Location
Orlando, FL
Type
conf
DOI
10.1109/ICUAS.2014.6842362
Filename
6842362
Link To Document