On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics

In this paper, a parameter uniform computational technique is examined for a partially singularly perturbed semi-linear system of equations which models the flight dynamics of an Unmanned Aerial Vehicle (UAV) and a Helicopter. The components of the solution of this system are expected to exhibit ove...

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Main Authors: K. Saravana Sankar, L. Jones Tarcius Doss
Format: Article
Language:English
Published: Elsevier 2023-03-01
Series:Results in Control and Optimization
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2666720723000103
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author K. Saravana Sankar
L. Jones Tarcius Doss
author_facet K. Saravana Sankar
L. Jones Tarcius Doss
author_sort K. Saravana Sankar
collection DOAJ
description In this paper, a parameter uniform computational technique is examined for a partially singularly perturbed semi-linear system of equations which models the flight dynamics of an Unmanned Aerial Vehicle (UAV) and a Helicopter. The components of the solution of this system are expected to exhibit overlapping boundary layers at the origin. To resolve the layers, a piecewise uniform Shishkin mesh is constructed so that a half of the mesh points are obtained in the layer region. The numerical method is proved to be parameter uniform and first order convergent. The method is tested for few numerical examples.
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spelling doaj.art-915c9980300649399981931a9ca133bb2023-03-09T04:13:54ZengElsevierResults in Control and Optimization2666-72072023-03-0110100208On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamicsK. Saravana Sankar0L. Jones Tarcius Doss1Department of Mathematics, CEG, Anna University, Chennai, 600025, Tamil Nadu, IndiaCorresponding author.; Department of Mathematics, CEG, Anna University, Chennai, 600025, Tamil Nadu, IndiaIn this paper, a parameter uniform computational technique is examined for a partially singularly perturbed semi-linear system of equations which models the flight dynamics of an Unmanned Aerial Vehicle (UAV) and a Helicopter. The components of the solution of this system are expected to exhibit overlapping boundary layers at the origin. To resolve the layers, a piecewise uniform Shishkin mesh is constructed so that a half of the mesh points are obtained in the layer region. The numerical method is proved to be parameter uniform and first order convergent. The method is tested for few numerical examples.http://www.sciencedirect.com/science/article/pii/S2666720723000103System of singularly perturbed equationsNon-linear controlUAV modelBoundary layersShishkin mesh
spellingShingle K. Saravana Sankar
L. Jones Tarcius Doss
On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
Results in Control and Optimization
System of singularly perturbed equations
Non-linear control
UAV model
Boundary layers
Shishkin mesh
title On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
title_full On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
title_fullStr On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
title_full_unstemmed On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
title_short On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
title_sort on parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics
topic System of singularly perturbed equations
Non-linear control
UAV model
Boundary layers
Shishkin mesh
url http://www.sciencedirect.com/science/article/pii/S2666720723000103
work_keys_str_mv AT ksaravanasankar onparameteruniformandlayerresolvingnumericalmethodforasingularlyperturbedmodelinaerodynamics
AT ljonestarciusdoss onparameteruniformandlayerresolvingnumericalmethodforasingularlyperturbedmodelinaerodynamics