Path following for unmanned helicopter: An approach on energy autonomy improvement
- Autores
- Gandolfo, Daniel; Salinas, Lucio Rafael; Toibero, Juan Marcos; Brandão, Alexandre
- Año de publicación
- 2016
- Idioma
- inglés
- Tipo de recurso
- artículo
- Estado
- versión publicada
- Descripción
- In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substantially in terms of control stabilization and navigation strategies. However, the energy available on board is finite and this is a limiting factor that prevents engineers from coming up with the best aerial solution in many situations. In this paper the path following control of a helicopter UAV based on the kinematic model is proposed using a feedback linearization technique. The helicopter speed is adjusted according to direction changes of the desired path. Thus, the aircraft should holds its own weight in the air for the shortest possible time, aiming to save energy without neglecting the position control errors which can accumulate when its velocity increases and path direction changes. The proposed controller output is coupled to a dynamic model of a helicopter in order to evaluate the dynamic effects and to adjust the controller parameters. The stability of the controller is demonstrated in the sense of Lyapunov theory and validated by simulation results.
Fil: Gandolfo, Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina
Fil: Salinas, Lucio Rafael. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina
Fil: Toibero, Juan Marcos. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina
Fil: Brandão, Alexandre. Universidad Federal de Viçosa; Brasil - Materia
-
PATH FOLLOWING CONTROLLER
POSITION CONTROL ERRORS
TRAVELED PATH
UNMANNED AERIAL VEHICLES - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- https://creativecommons.org/licenses/by/2.5/ar/
- Repositorio
- Institución
- Consejo Nacional de Investigaciones Científicas y Técnicas
- OAI Identificador
- oai:ri.conicet.gov.ar:11336/56889
Ver los metadatos del registro completo
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Path following for unmanned helicopter: An approach on energy autonomy improvementGandolfo, DanielSalinas, Lucio RafaelToibero, Juan MarcosBrandão, AlexandrePATH FOLLOWING CONTROLLERPOSITION CONTROL ERRORSTRAVELED PATHUNMANNED AERIAL VEHICLEShttps://purl.org/becyt/ford/2.2https://purl.org/becyt/ford/2In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substantially in terms of control stabilization and navigation strategies. However, the energy available on board is finite and this is a limiting factor that prevents engineers from coming up with the best aerial solution in many situations. In this paper the path following control of a helicopter UAV based on the kinematic model is proposed using a feedback linearization technique. The helicopter speed is adjusted according to direction changes of the desired path. Thus, the aircraft should holds its own weight in the air for the shortest possible time, aiming to save energy without neglecting the position control errors which can accumulate when its velocity increases and path direction changes. The proposed controller output is coupled to a dynamic model of a helicopter in order to evaluate the dynamic effects and to adjust the controller parameters. The stability of the controller is demonstrated in the sense of Lyapunov theory and validated by simulation results.Fil: Gandolfo, Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; ArgentinaFil: Salinas, Lucio Rafael. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; ArgentinaFil: Toibero, Juan Marcos. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; ArgentinaFil: Brandão, Alexandre. Universidad Federal de Viçosa; BrasilKaunas University of Technology2016-03info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/56889Gandolfo, Daniel; Salinas, Lucio Rafael; Toibero, Juan Marcos; Brandão, Alexandre; Path following for unmanned helicopter: An approach on energy autonomy improvement; Kaunas University of Technology; Information Technology and Control; 45; 1; 3-2016; 86-981392-124X2335-884XCONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.5755/j01.itc.45.1.12413info:eu-repo/semantics/altIdentifier/url/http://www.itc.ktu.lt/index.php/ITC/article/view/12413info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-09-29T10:40:59Zoai:ri.conicet.gov.ar:11336/56889instacron:CONICETInstitucionalhttp://ri.conicet.gov.ar/Organismo científico-tecnológicoNo correspondehttp://ri.conicet.gov.ar/oai/requestdasensio@conicet.gov.ar; lcarlino@conicet.gov.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:34982025-09-29 10:40:59.692CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse |
dc.title.none.fl_str_mv |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
title |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
spellingShingle |
Path following for unmanned helicopter: An approach on energy autonomy improvement Gandolfo, Daniel PATH FOLLOWING CONTROLLER POSITION CONTROL ERRORS TRAVELED PATH UNMANNED AERIAL VEHICLES |
title_short |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
title_full |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
title_fullStr |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
title_full_unstemmed |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
title_sort |
Path following for unmanned helicopter: An approach on energy autonomy improvement |
dc.creator.none.fl_str_mv |
Gandolfo, Daniel Salinas, Lucio Rafael Toibero, Juan Marcos Brandão, Alexandre |
author |
Gandolfo, Daniel |
author_facet |
Gandolfo, Daniel Salinas, Lucio Rafael Toibero, Juan Marcos Brandão, Alexandre |
author_role |
author |
author2 |
Salinas, Lucio Rafael Toibero, Juan Marcos Brandão, Alexandre |
author2_role |
author author author |
dc.subject.none.fl_str_mv |
PATH FOLLOWING CONTROLLER POSITION CONTROL ERRORS TRAVELED PATH UNMANNED AERIAL VEHICLES |
topic |
PATH FOLLOWING CONTROLLER POSITION CONTROL ERRORS TRAVELED PATH UNMANNED AERIAL VEHICLES |
purl_subject.fl_str_mv |
https://purl.org/becyt/ford/2.2 https://purl.org/becyt/ford/2 |
dc.description.none.fl_txt_mv |
In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substantially in terms of control stabilization and navigation strategies. However, the energy available on board is finite and this is a limiting factor that prevents engineers from coming up with the best aerial solution in many situations. In this paper the path following control of a helicopter UAV based on the kinematic model is proposed using a feedback linearization technique. The helicopter speed is adjusted according to direction changes of the desired path. Thus, the aircraft should holds its own weight in the air for the shortest possible time, aiming to save energy without neglecting the position control errors which can accumulate when its velocity increases and path direction changes. The proposed controller output is coupled to a dynamic model of a helicopter in order to evaluate the dynamic effects and to adjust the controller parameters. The stability of the controller is demonstrated in the sense of Lyapunov theory and validated by simulation results. Fil: Gandolfo, Daniel. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina Fil: Salinas, Lucio Rafael. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina Fil: Toibero, Juan Marcos. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - San Juan. Instituto de Automática. Universidad Nacional de San Juan. Facultad de Ingeniería. Instituto de Automática; Argentina Fil: Brandão, Alexandre. Universidad Federal de Viçosa; Brasil |
description |
In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substantially in terms of control stabilization and navigation strategies. However, the energy available on board is finite and this is a limiting factor that prevents engineers from coming up with the best aerial solution in many situations. In this paper the path following control of a helicopter UAV based on the kinematic model is proposed using a feedback linearization technique. The helicopter speed is adjusted according to direction changes of the desired path. Thus, the aircraft should holds its own weight in the air for the shortest possible time, aiming to save energy without neglecting the position control errors which can accumulate when its velocity increases and path direction changes. The proposed controller output is coupled to a dynamic model of a helicopter in order to evaluate the dynamic effects and to adjust the controller parameters. The stability of the controller is demonstrated in the sense of Lyapunov theory and validated by simulation results. |
publishDate |
2016 |
dc.date.none.fl_str_mv |
2016-03 |
dc.type.none.fl_str_mv |
info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion http://purl.org/coar/resource_type/c_6501 info:ar-repo/semantics/articulo |
format |
article |
status_str |
publishedVersion |
dc.identifier.none.fl_str_mv |
http://hdl.handle.net/11336/56889 Gandolfo, Daniel; Salinas, Lucio Rafael; Toibero, Juan Marcos; Brandão, Alexandre; Path following for unmanned helicopter: An approach on energy autonomy improvement; Kaunas University of Technology; Information Technology and Control; 45; 1; 3-2016; 86-98 1392-124X 2335-884X CONICET Digital CONICET |
url |
http://hdl.handle.net/11336/56889 |
identifier_str_mv |
Gandolfo, Daniel; Salinas, Lucio Rafael; Toibero, Juan Marcos; Brandão, Alexandre; Path following for unmanned helicopter: An approach on energy autonomy improvement; Kaunas University of Technology; Information Technology and Control; 45; 1; 3-2016; 86-98 1392-124X 2335-884X CONICET Digital CONICET |
dc.language.none.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
info:eu-repo/semantics/altIdentifier/doi/10.5755/j01.itc.45.1.12413 info:eu-repo/semantics/altIdentifier/url/http://www.itc.ktu.lt/index.php/ITC/article/view/12413 |
dc.rights.none.fl_str_mv |
info:eu-repo/semantics/openAccess https://creativecommons.org/licenses/by/2.5/ar/ |
eu_rights_str_mv |
openAccess |
rights_invalid_str_mv |
https://creativecommons.org/licenses/by/2.5/ar/ |
dc.format.none.fl_str_mv |
application/pdf application/pdf application/pdf application/pdf |
dc.publisher.none.fl_str_mv |
Kaunas University of Technology |
publisher.none.fl_str_mv |
Kaunas University of Technology |
dc.source.none.fl_str_mv |
reponame:CONICET Digital (CONICET) instname:Consejo Nacional de Investigaciones Científicas y Técnicas |
reponame_str |
CONICET Digital (CONICET) |
collection |
CONICET Digital (CONICET) |
instname_str |
Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.name.fl_str_mv |
CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.mail.fl_str_mv |
dasensio@conicet.gov.ar; lcarlino@conicet.gov.ar |
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1844614439813251072 |
score |
13.070432 |