Observer based rotor failure compensation for biplane quadrotor with slung load

In this study, mathematical modeling of biplane quadrotor with slung load is proposed. Performance of the biplane quadrotor is degrade while swinging of the slung load so to compensate it nonlinear observer based backstepping controller is designed that can not only handle the disturbance generated...

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Main Authors: Nihal Dalwadi, Dipankar Deb, S.M. Muyeen
Format: Article
Language:English
Published: Elsevier 2022-11-01
Series:Ain Shams Engineering Journal
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2090447922000594
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author Nihal Dalwadi
Dipankar Deb
S.M. Muyeen
author_facet Nihal Dalwadi
Dipankar Deb
S.M. Muyeen
author_sort Nihal Dalwadi
collection DOAJ
description In this study, mathematical modeling of biplane quadrotor with slung load is proposed. Performance of the biplane quadrotor is degrade while swinging of the slung load so to compensate it nonlinear observer based backstepping controller is designed that can not only handle the disturbance generated by the slung load but can also capable to tackle partial rotor failure and wind gust. Simulation study carried out by considering slung load swinging (only for quadrotor mode), wind gust, and rotor failure (for all three modes) as the external disturbance and nonlinear observer is design to estimate it. Backstepping control technique is used to design controller for all three modes of biplane quadrotor. Simulation study shows that proposed control scheme is cable to handle the disturbance generated by the different sources in quadrotor biplane.
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spelling doaj.art-b029593a6dad44c69a82f4c124c124292022-12-22T04:41:31ZengElsevierAin Shams Engineering Journal2090-44792022-11-01136101748Observer based rotor failure compensation for biplane quadrotor with slung loadNihal Dalwadi0Dipankar Deb1S.M. Muyeen2Department of Electrical Engineering, Institute of Infrastructure Technology, Research and Management, Ahmedabad 380026, IndiaDepartment of Electrical Engineering, Institute of Infrastructure Technology, Research and Management, Ahmedabad 380026, IndiaDepartment of Electrical Engineering, Qatar University, Doha 2713, Qatar; Corresponding author.In this study, mathematical modeling of biplane quadrotor with slung load is proposed. Performance of the biplane quadrotor is degrade while swinging of the slung load so to compensate it nonlinear observer based backstepping controller is designed that can not only handle the disturbance generated by the slung load but can also capable to tackle partial rotor failure and wind gust. Simulation study carried out by considering slung load swinging (only for quadrotor mode), wind gust, and rotor failure (for all three modes) as the external disturbance and nonlinear observer is design to estimate it. Backstepping control technique is used to design controller for all three modes of biplane quadrotor. Simulation study shows that proposed control scheme is cable to handle the disturbance generated by the different sources in quadrotor biplane.http://www.sciencedirect.com/science/article/pii/S2090447922000594Biplane quadrotorSlung loadNonlinear Observer designPartial Rotor failureWind gustTrajectory tracking
spellingShingle Nihal Dalwadi
Dipankar Deb
S.M. Muyeen
Observer based rotor failure compensation for biplane quadrotor with slung load
Ain Shams Engineering Journal
Biplane quadrotor
Slung load
Nonlinear Observer design
Partial Rotor failure
Wind gust
Trajectory tracking
title Observer based rotor failure compensation for biplane quadrotor with slung load
title_full Observer based rotor failure compensation for biplane quadrotor with slung load
title_fullStr Observer based rotor failure compensation for biplane quadrotor with slung load
title_full_unstemmed Observer based rotor failure compensation for biplane quadrotor with slung load
title_short Observer based rotor failure compensation for biplane quadrotor with slung load
title_sort observer based rotor failure compensation for biplane quadrotor with slung load
topic Biplane quadrotor
Slung load
Nonlinear Observer design
Partial Rotor failure
Wind gust
Trajectory tracking
url http://www.sciencedirect.com/science/article/pii/S2090447922000594
work_keys_str_mv AT nihaldalwadi observerbasedrotorfailurecompensationforbiplanequadrotorwithslungload
AT dipankardeb observerbasedrotorfailurecompensationforbiplanequadrotorwithslungload
AT smmuyeen observerbasedrotorfailurecompensationforbiplanequadrotorwithslungload