Quadcopter UAV Control based on Input-Output Linearization and PID

J. Aguerrebere, E. G. Hernandez-Martinez, S. Montufar-Chavez, X. Tortolero-Baena, M. Salgado-Aguirre, G. Fernandez-Anaya, E. Ferreira-Vazquez, J. J. Flores-Godoy

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A dynamical model of the quadcopter UAV is obtained considering the frictional effects in the positional and rotational coordinates. Then, a two-level control strategy is designed using an input-output Linearization in combination with PID controllers. The inner loop stabilizes the pitch, roll and yaw angles, whilst the outer-loop control is related to the position control, avoiding local Linearization. A PID control gain selection is analyzed to harmonize both control loops. The performance of the control approach is shown by numerical simulations.

Original languageEnglish
Title of host publication2021 IEEE International Midwest Symposium on Circuits and Systems, MWSCAS 2021 - Proceedings
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1003-1006
Number of pages4
ISBN (Electronic)9781665424615
DOIs
StatePublished - 9 Aug 2021
Event2021 IEEE International Midwest Symposium on Circuits and Systems, MWSCAS 2021 - Virtual, East Lansing, United States
Duration: 9 Aug 202111 Aug 2021

Publication series

NameMidwest Symposium on Circuits and Systems
Volume2021-August
ISSN (Print)1548-3746

Conference

Conference2021 IEEE International Midwest Symposium on Circuits and Systems, MWSCAS 2021
Country/TerritoryUnited States
CityVirtual, East Lansing
Period9/08/2111/08/21

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