Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba

Castillo, Oscar Daniel Garibaldi; Beltrán, Ana; Castillo, Oscar Daniel Garibaldi; Beltrán, Ana

dc.contributor		en-US
dc.creator	Castillo, Oscar Daniel Garibaldi
dc.creator	Beltrán, Ana
dc.creator	Castillo, Oscar Daniel Garibaldi
dc.creator	Beltrán, Ana
dc.date	2018-02-11
dc.date.accessioned	2018-02-23T17:16:28Z
dc.date.available	2018-02-23T17:16:28Z
dc.identifier	https://knepublishing.com/index.php/KnE-Engineering/article/view/1452
dc.identifier	10.18502/keg.v3i1.1452
dc.identifier.uri	http://ridda2.utp.ac.pa/handle/123456789/4341
dc.description	The design and implementation of a autonomous navigation and control system for UAV, mandates simulating the system before in-flight testing. These simulations require a computational model of the aircraft, that can be obtained from the computation of aerodynamic parameters such as the drag polar. In this paper we present the identification of these parameters using two methods: one by flight testing techniques; the other by a combination of semi-empirical methods and computational fluid dynamics, dubbed the hybrid method. The hybrid method, which produces a parabolic polar drag, had the same qualitative trend compared to experiments. However, a detailed analysis of the parameters that shapes the polar drag, had significant differences, particularly in the parasite drag. This is probably due to propeller effects, low Reynolds Number and limitations of the piloting technique.Keywords: Drag polar, flight testing, parasite drag, UAV, VLM	en-US
dc.format	application/msword
dc.format	application/pdf
dc.format	application/xml
dc.language	eng
dc.publisher	KnE Publishing	en-US
dc.relation	https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3262
dc.relation	https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3507
dc.relation	https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3508
dc.rights	info:eu-repo/semantics/openAccess
dc.rights	https://creativecommons.org/licenses/by/4.0/
dc.source	2518-6841
dc.source	KnE Engineering; 6th Engineering, Science and Technology Conference - Panama 2017 (ESTEC 2017); 482-491	en-US
dc.title	Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba	en-US
dc.type	info:eu-repo/semantics/article
dc.type	info:eu-repo/semantics/publishedVersion

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2017: 6th Engineering, Science and Technology Conference - Panama (ESTEC 2017) [115]
6th Engineering, Science and Technology Conference (ESTEC 2017) organized by the Universidad Tecnologica de Panama (UTP)

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