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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University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2017-01-01
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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 |
_version_ |
1724506978503360512 |