Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts

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When you want to develop and test software products for complex systems such as airplanes, space shuttles, satellites, automobiles or nuclear plants, one of the biggest drawbacks is the availability of the physical system, due to the great complexity, risks and costs involved in performing tests on...

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Detalles Bibliográficos
Autor: Quiroz Villalobos, Lennin Paul
Formato: artículo
Fecha de Publicación:2020
Institución:Universidad de Lima
Repositorio:Revistas - Universidad de Lima
Lenguaje:español
OAI Identifier:oai:revistas.ulima.edu.pe:article/4857
Enlace del recurso:https://revistas.ulima.edu.pe/index.php/Interfases/article/view/4857
Nivel de acceso:acceso abierto
Materia:SITL
autopilot
aircrafts
Software Engineering
Simulink
PID
piloto automático
aeronaves
ingeniería de software
simulink
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network_name_str Revistas - Universidad de Lima
repository_id_str
spelling Software in the Loop for the implementation of an autopilot system for fixed-wing aircraftsSoftware in the Loop para la implementación de un sistema de piloto automático para aeronaves de ala fijaQuiroz Villalobos, Lennin PaulSITLautopilotaircraftsSoftware EngineeringSimulinkPIDSITLpiloto automáticoaeronavesingeniería de softwaresimulinkPIDWhen you want to develop and test software products for complex systems such as airplanes, space shuttles, satellites, automobiles or nuclear plants, one of the biggest drawbacks is the availability of the physical system, due to the great complexity, risks and costs involved in performing tests on the real system. Software in the Loop (SITL) allows us to test algorithms, source code or control strategies for complex systems within a simulation that contains the mathematical model of the real physical system. This research work proposes the use of a Software in the Loop platform for the development of an autopilot system for a fixed-wing aircraft. The architecture of the implemented application, the software design process, the protocols used, the control strategies, the programming techniques, the results obtained and the conclusions are shown herein.Cuando se desea desarrollar y probar softwares para sistemas complejos, como aviones, transbordadores espaciales, satélites, automóviles o plantas nucleares, uno de los mayores inconvenientes es la gran complejidad, riesgos y costos que implica realizar pruebas sobre el sistema real. Software in the Loop (SITL) permite testear algoritmos, códigos fuente o estrategias de control para sistemas complejos dentro de una simulación que contiene el modelo matemático del sistema físico real. El presente trabajo propone el uso de la plataforma Software in the Loop con el fin de desarrollar un sistema de piloto automático para una aeronave de ala fija. Se muestra la arquitectura de la aplicación implementada, el proceso de diseño de software, los protocolos utilizados, las estrategias de control, técnicas de programación, los resultados obtenidos y las conclusiones.Universidad de Lima2020-12-22info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfhttps://revistas.ulima.edu.pe/index.php/Interfases/article/view/485710.26439/interfases2020.n013.4857Interfases; No. 013 (2020); 39-56Interfases; Núm. 013 (2020); 39-56Interfases; n. 013 (2020); 39-561993-491210.26439/interfases2020.n013reponame:Revistas - Universidad de Limainstname:Universidad de Limainstacron:ULIMAspahttps://revistas.ulima.edu.pe/index.php/Interfases/article/view/4857/4870Derechos de autor 2020 Revista Interfaseshttps://creativecommons.org/licenses/by-nd/4.0info:eu-repo/semantics/openAccessoai:revistas.ulima.edu.pe:article/48572023-07-24T13:32:54Z
dc.title.none.fl_str_mv Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
Software in the Loop para la implementación de un sistema de piloto automático para aeronaves de ala fija
title Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
spellingShingle Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
Quiroz Villalobos, Lennin Paul
SITL
autopilot
aircrafts
Software Engineering
Simulink
PID
SITL
piloto automático
aeronaves
ingeniería de software
simulink
PID
title_short Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
title_full Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
title_fullStr Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
title_full_unstemmed Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
title_sort Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
dc.creator.none.fl_str_mv Quiroz Villalobos, Lennin Paul
author Quiroz Villalobos, Lennin Paul
author_facet Quiroz Villalobos, Lennin Paul
author_role author
dc.subject.none.fl_str_mv SITL
autopilot
aircrafts
Software Engineering
Simulink
PID
SITL
piloto automático
aeronaves
ingeniería de software
simulink
PID
topic SITL
autopilot
aircrafts
Software Engineering
Simulink
PID
SITL
piloto automático
aeronaves
ingeniería de software
simulink
PID
description When you want to develop and test software products for complex systems such as airplanes, space shuttles, satellites, automobiles or nuclear plants, one of the biggest drawbacks is the availability of the physical system, due to the great complexity, risks and costs involved in performing tests on the real system. Software in the Loop (SITL) allows us to test algorithms, source code or control strategies for complex systems within a simulation that contains the mathematical model of the real physical system. This research work proposes the use of a Software in the Loop platform for the development of an autopilot system for a fixed-wing aircraft. The architecture of the implemented application, the software design process, the protocols used, the control strategies, the programming techniques, the results obtained and the conclusions are shown herein.
publishDate 2020
dc.date.none.fl_str_mv 2020-12-22
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.none.fl_str_mv https://revistas.ulima.edu.pe/index.php/Interfases/article/view/4857
10.26439/interfases2020.n013.4857
url https://revistas.ulima.edu.pe/index.php/Interfases/article/view/4857
identifier_str_mv 10.26439/interfases2020.n013.4857
dc.language.none.fl_str_mv spa
language spa
dc.relation.none.fl_str_mv https://revistas.ulima.edu.pe/index.php/Interfases/article/view/4857/4870
dc.rights.none.fl_str_mv Derechos de autor 2020 Revista Interfases
https://creativecommons.org/licenses/by-nd/4.0
info:eu-repo/semantics/openAccess
rights_invalid_str_mv Derechos de autor 2020 Revista Interfases
https://creativecommons.org/licenses/by-nd/4.0
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Universidad de Lima
publisher.none.fl_str_mv Universidad de Lima
dc.source.none.fl_str_mv Interfases; No. 013 (2020); 39-56
Interfases; Núm. 013 (2020); 39-56
Interfases; n. 013 (2020); 39-56
1993-4912
10.26439/interfases2020.n013
reponame:Revistas - Universidad de Lima
instname:Universidad de Lima
instacron:ULIMA
instname_str Universidad de Lima
instacron_str ULIMA
institution ULIMA
reponame_str Revistas - Universidad de Lima
collection Revistas - Universidad de Lima
repository.name.fl_str_mv
repository.mail.fl_str_mv
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Software in the Loop for the implementation of an autopilot system for fixed-wing aircrafts
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