Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling

In this paper, a novel fuzzy identification method for dynamic modelling of quadrotors UAV is presented. The method is based on a special parameterization of the antecedent part of fuzzy systems that results in fuzzy-partitions for antecedents. This antecedent parameter representation method of fuzz...

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Main Authors: Nemes Attila, Mester Gyula
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2017-01-01
Series:FME Transactions
Subjects:
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2017/1451-20921701001N.pdf
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spelling doaj-04ca230719b24815a369ed1f1abe46c52020-11-25T03:46:14ZengUniversity of Belgrade - Faculty of Mechanical Engineering, BelgradeFME Transactions1451-20922406-128X2017-01-01451181451-20921701001NUnconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modelingNemes Attila0Mester Gyula1https://orcid.org/0000-0001-7796-2820Óbuda University, Doctoral School of Safety and Security Sciences, Budapest, HungaryÓbuda University, Doctoral School of Safety and Security Sciences, Budapest, HungaryIn this paper, a novel fuzzy identification method for dynamic modelling of quadrotors UAV is presented. The method is based on a special parameterization of the antecedent part of fuzzy systems that results in fuzzy-partitions for antecedents. This antecedent parameter representation method of fuzzy rules ensures upholding of predefined linguistic value ordering and ensures that fuzzy-partitions remain intact throughout an unconstrained hybrid evolutionary and gradient descent based optimization process. In the equations of motion the first order derivative component is calculated based on Christoffel symbols, the derivatives of fuzzy systems are used for modelling the Coriolis effects, gyroscopic and centrifugal terms. The non-linear parameters are subjected to an initial global evolutionary optimization scheme and fine tuning with gradient descent based local search. Simulation results of the proposed new quadrotor dynamic model identification method are promising.https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2017/1451-20921701001N.pdffuzzy identification methoddynamic modellingquadrotor uavchristoffel symbolsgenetic algorithmsnon-linear parametersglobal evolutionary optimization
collection DOAJ
language English
format Article
sources DOAJ
author Nemes Attila
Mester Gyula
spellingShingle Nemes Attila
Mester Gyula
Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
FME Transactions
fuzzy identification method
dynamic modelling
quadrotor uav
christoffel symbols
genetic algorithms
non-linear parameters
global evolutionary optimization
author_facet Nemes Attila
Mester Gyula
author_sort Nemes Attila
title Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
title_short Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
title_full Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
title_fullStr Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
title_full_unstemmed Unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for UAV dynamic modeling
title_sort unconstrained evolutionary and gradient descent-based tuning of fuzzy-partitions for uav dynamic modeling
publisher University of Belgrade - Faculty of Mechanical Engineering, Belgrade
series FME Transactions
issn 1451-2092
2406-128X
publishDate 2017-01-01
description In this paper, a novel fuzzy identification method for dynamic modelling of quadrotors UAV is presented. The method is based on a special parameterization of the antecedent part of fuzzy systems that results in fuzzy-partitions for antecedents. This antecedent parameter representation method of fuzzy rules ensures upholding of predefined linguistic value ordering and ensures that fuzzy-partitions remain intact throughout an unconstrained hybrid evolutionary and gradient descent based optimization process. In the equations of motion the first order derivative component is calculated based on Christoffel symbols, the derivatives of fuzzy systems are used for modelling the Coriolis effects, gyroscopic and centrifugal terms. The non-linear parameters are subjected to an initial global evolutionary optimization scheme and fine tuning with gradient descent based local search. Simulation results of the proposed new quadrotor dynamic model identification method are promising.
topic fuzzy identification method
dynamic modelling
quadrotor uav
christoffel symbols
genetic algorithms
non-linear parameters
global evolutionary optimization
url https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2017/1451-20921701001N.pdf
work_keys_str_mv AT nemesattila unconstrainedevolutionaryandgradientdescentbasedtuningoffuzzypartitionsforuavdynamicmodeling
AT mestergyula unconstrainedevolutionaryandgradientdescentbasedtuningoffuzzypartitionsforuavdynamicmodeling
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