Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba
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....
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| Jazyk: | angličtina |
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2018
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| On-line přístup: | https://knepublishing.com/index.php/KnE-Engineering/article/view/1452 http://ridda2.utp.ac.pa/handle/123456789/4341 |
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| _version_ | 1869652474735886336 |
|---|---|
| author | Castillo, Oscar Daniel Garibaldi |
| author2 | Beltrán, Ana |
| author2_role | author |
| author_browse | Beltrán, Ana Castillo, Oscar Daniel Garibaldi |
| author_facet | Castillo, Oscar Daniel Garibaldi Beltrán, Ana |
| author_role | author |
| collection | Repositorio Institucional de documento digitales de acceso abierto de la UTP |
| dc.contributor.none.fl_str_mv | |
| dc.creator.none.fl_str_mv | Castillo, Oscar Daniel Garibaldi Beltrán, Ana Castillo, Oscar Daniel Garibaldi Beltrán, Ana |
| dc.date.none.fl_str_mv | 2018-02-11 2018-02-23T17:16:28Z 2018-02-23T17:16:28Z |
| dc.format.none.fl_str_mv | application/msword application/pdf application/xml |
| dc.identifier.none.fl_str_mv | https://knepublishing.com/index.php/KnE-Engineering/article/view/1452 10.18502/keg.v3i1.1452 http://ridda2.utp.ac.pa/handle/123456789/4341 |
| dc.language.none.fl_str_mv | eng |
| dc.publisher.none.fl_str_mv | KnE Publishing |
| dc.relation.none.fl_str_mv | https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3262 https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3507 https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3508 |
| dc.rights.none.fl_str_mv | info:eu-repo/semantics/openAccess https://creativecommons.org/licenses/by/4.0/ |
| dc.source.none.fl_str_mv | 2518-6841 KnE Engineering; 6th Engineering, Science and Technology Conference - Panama 2017 (ESTEC 2017); 482-491 reponame:Repositorio Institucional de documento digitales de acceso abierto de la UTP instname:Universidad Tecnológica de Panamá instacron:U Tecnológica de Panamá |
| dc.title.none.fl_str_mv | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| dc.type.none.fl_str_mv | info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion |
| 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 |
| eu_rights_str_mv | openAccess |
| format | article |
| id | lrtest_c6197f77323696bf8a9ed8d595e25c23 |
| identifier_str_mv | 10.18502/keg.v3i1.1452 |
| instacron_str | U Tecnológica de Panamá |
| institution | U Tecnológica de Panamá |
| instname_str | Universidad Tecnológica de Panamá |
| language | eng |
| network_acronym_str | lrtest |
| network_name_str | lr |
| oai_identifier_str | oai:ridda2.utp.ac.pa:123456789/4341 |
| publishDate | 2018 |
| publishDateSort | 2018 |
| publisher.none.fl_str_mv | KnE Publishing |
| reponame_str | Repositorio Institucional de documento digitales de acceso abierto de la UTP |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| rights_invalid_str_mv | https://creativecommons.org/licenses/by/4.0/ |
| spelling | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de PruebaCastillo, Oscar Daniel GaribaldiBeltrán, AnaCastillo, Oscar Daniel GaribaldiBeltrán, AnaThe 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, VLMKnE Publishing2018-02-112018-02-23T17:16:28Z2018-02-23T17:16:28Zinfo:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/mswordapplication/pdfapplication/xmlhttps://knepublishing.com/index.php/KnE-Engineering/article/view/145210.18502/keg.v3i1.1452http://ridda2.utp.ac.pa/handle/123456789/43412518-6841KnE Engineering; 6th Engineering, Science and Technology Conference - Panama 2017 (ESTEC 2017); 482-491reponame:Repositorio Institucional de documento digitales de acceso abierto de la UTPinstname:Universidad Tecnológica de Panamáinstacron:U Tecnológica de Panamáenghttps://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3262https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3507https://knepublishing.com/index.php/KnE-Engineering/article/view/1452/3508info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by/4.0/oai:ridda2.utp.ac.pa:123456789/43412021-07-06T16:47:38Z |
| spellingShingle | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba Castillo, Oscar Daniel Garibaldi |
| status_str | publishedVersion |
| title | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| title_full | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| title_fullStr | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| title_full_unstemmed | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| title_short | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| title_sort | Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba |
| url | https://knepublishing.com/index.php/KnE-Engineering/article/view/1452 http://ridda2.utp.ac.pa/handle/123456789/4341 |