DocumentCode
720466
Title
Quadrotor control in a wind field
Author
Nguyen Khoi Tran ; Bulka, Eitan ; Nahon, Meyer
Author_Institution
Dept. of Mech. Eng., McGill Univ., Montreal, QC, Canada
fYear
2015
fDate
9-12 June 2015
Firstpage
320
Lastpage
328
Abstract
This paper investigates the ability of a quadrotor to maneuver in a wind field. A dynamic model of a quadrotor is presented to model its motion. The quadrotor model includes a wind effect model to quantify the effect of wind on the dynamics of a quadrotor. A proportional-integral-derivative (PID) controller is shown as a baseline controller typically used on quadrotors. A LQR controller is then shown as an alternative to a PID controller. These two controllers are compared in a simulation environment using the wind effect model and simulated wind disturbances. Both controllers are found to have similar performance in a wind field, though the LQR controller is found to be easier to tune.
Keywords
aerodynamics; aircraft control; flow control; helicopters; linear quadratic control; motion control; three-term control; vehicle dynamics; wind; LQR controller; PID controller; linear quadratic regulator control; maneuver; motion modeling; proportional-integral-derivative controller; quadrotor control; quadrotor dynamic model; quadrotor model; wind disturbances; wind effect model; wind field; Atmospheric modeling; Force; Mathematical model; Predictive models; Propellers; Wind forecasting;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
Conference_Location
Denver, CO
Print_ISBN
978-1-4799-6009-5
Type
conf
DOI
10.1109/ICUAS.2015.7152306
Filename
7152306
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