PID, LQR and LQR-PID on a quadcopter platform

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dc.contributor.authorAGENTIM, L. M.
dc.contributor.authorREZENDE, W. C.
dc.contributor.authorPaulo Santos
dc.contributor.authorRenato Aguiar
dc.contributor.authorOrcidhttps://orcid.org/0000-0001-8484-0354
dc.contributor.authorOrcidhttps://orcid.org/0000-0002-4413-3847
dc.date.accessioned2022-01-12T22:01:25Z
dc.date.available2022-01-12T22:01:25Z
dc.date.issued2013-05-17
dc.description.abstractThis paper aims to present a comparison between different controllers to be used in a dynamic model of a quadcopter platform. The controllers assumed in this work are an ITAE tuned PID, a classic LQR controller and a PID tuned with a LQR loop. The results were obtained through simulations for 10 different attitudes of the quadcopter, however, in this paper simulation results will be presented for the vertical attitude only (the remainder are analogous and were omitted for brevity). © 2013 IEEE.
dc.identifier.citationAGENTIM, L. M.; REZENDE, W. C.; SANTOS, P. E.; AGUIAR, R. A. PID, LQR and LQR-PID on a quadcopter platform. 2013 International Conference on Informatics, Electronics and Vision, ICIEV 2013, Mayo, 2013.
dc.identifier.doi10.1109/ICIEV.2013.6572698
dc.identifier.urihttps://repositorio.fei.edu.br/handle/FEI/4066
dc.relation.ispartof2013 International Conference on Informatics, Electronics and Vision, ICIEV 2013
dc.rightsAcesso Restrito
dc.titlePID, LQR and LQR-PID on a quadcopter platform
dc.typeArtigo de evento
fei.scopus.citations158
fei.scopus.eid2-s2.0-84883316055
fei.scopus.subjectLQR controller
fei.scopus.updated2024-07-01
fei.scopus.urlhttps://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84883316055&origin=inward
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