Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5906
Title: Quadrotor roll and pitch stabilization using system identification based redesign of empirical controllers
Authors: Batmaz, Anıl Ufuk
Elbir O.
Kasnakoğlu, Coşku
Keywords: Aerial vehicles
Discrete time
Four rotor helicopter
Linear estimation
Quadrotor
UAV
Vehicle control
Issue Date: 2013
Source: 32nd IASTED International Conference on Modelling, Identification and Control, MIC 2013, 11 February 2013 through 13 February 2013, Innsbruck, 96248
Abstract: Unmanned Aerial Vehicles (UAVs) are currently one of the hot topics of study which have numerous applications such as remote sensing, aerial surveillance, exploration, search and rescue, transport, scientific research and armed attacks. In this work we consider a test-bed for the design of a low cost flight controller for a quadrotor and we demonstrate the design of the roll and pitch controllers on an experimental setup through the stages of data collection, modeling, control design and verification. The procedure consists of four stages: 1) Experimental determination of controller coefficients, 2) Data collection, 3) System identification, 4) Controller redesign by tuning coefficients with a numerical search. It is observed that the system designed as such is capable of achieving satisfactory pitch and roll stabilization, and coefficient tuning on the identified model noticeably improves the settling time and steady state oscillation amplitude.
URI: https://doi.org/10.2316/P.2013.794-060
https://hdl.handle.net/20.500.11851/5906
ISBN: 9780889869431
ISSN: 1025-8973
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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