DocumentCode
261623
Title
Full linear control of a quadrotor UAV, LQ vs H∞
Author
Araar, Oualid ; Aouf, Nabil
Author_Institution
Centre for Electron. Warfare, Cranfield Univ., Shrivenham, UK
fYear
2014
fDate
9-11 July 2014
Firstpage
133
Lastpage
138
Abstract
Quadrotors low level control has attracted the attention of many research works over the last decade. In most of previous works, position stabilisation was achieved using nonlinear control techniques. In this paper, two full linear techniques based on optimal control theory are presented. The first, based on the L2 norm, is a Linear Quadratique Servo (LQ-Servo) controller. The second one, optimizes the L∞ norm and is designed using H∞ control approach. Emphasis is placed on the robustness to external disturbances and particularly wind gusts. Simulation results based on the full nonlinear model of the quadrotor are presented as a basis of comparison between the two controllers.
Keywords
H∞ control; autonomous aerial vehicles; control system synthesis; helicopters; linear quadratic control; mobile robots; optimisation; position control; robust control; servomechanisms; H∞ control; L∞ norm optimization; L2 norm; LQ-servo controller; UAV; control system design; linear quadratique servo; optimal control theory; position stabilisation; quadrotor linear control; robustness; Equations; Mathematical model; Robustness; Trajectory; Vectors; Vehicle dynamics; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Control (CONTROL), 2014 UKACC International Conference on
Conference_Location
Loughborough
Type
conf
DOI
10.1109/CONTROL.2014.6915128
Filename
6915128
Link To Document