Simulation and experimental study on attitude control of quadrotor

Conference proceedings article

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Publication Details

Author list: Trirattanawananon N., Panomruttanarug B., Higuchi K., Mora-Camino F.

Publisher: Hindawi

Publication year: 2014

Start page: 1719

End page: 1724

Number of pages: 6

ISBN: 9781479973965

ISSN: 0146-9428

eISSN: 1745-4557

URL: https://www.scopus.com/inward/record.uri?eid=2-s2.0-84949926916&doi=10.1109%2fROBIO.2014.7090583&partnerID=40&md5=d183cffe77e326807917849d7e689706

Languages: English-Great Britain (EN-GB)

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Abstract

This paper studies dynamic behavior of a quadrotor in both simulation and experiment when tracking desired attitude angles. The flight attitude control implemented in this research is designed based on a feedback control with an inner-loop structure as in the Aeroquad project. The feedback control configuration is applied to the dynamic model of a DIY qaudrotor UAV to simulate its attitude tracking behavior when tuning the PID gains based on a heuristic approach. The well-tuned PID controller is therefore applied to the experiment to validate the desired tracking response. ฉ 2014 IEEE.

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