Minimum-energy path generation for a quadrotor UAV

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AudienciaPúblico en generales_ES
CoberturaMéxico[ 143]es_ES
Fecha de ingreso2026-10-05T16:35:05Z
Fecha de publicación2016-01-01
ResumenA major limitation of existing battery-powered quadrotor UAVs is their reduced flight endurance. To address this issue, by leveraging the electrical model of a brushless DC motor, we explicitly determine minimum-energy paths between a predefined initial and final configuration of a quadrotor by solving an optimal control problem with respect to the angular accelerations of the four propellers. As a variation on this problem, if the total energy consumption between two boundary states is fixed, minimum-time and/or minimum-control-effort trajectories are computed for the aerial vehicle. The theory is illustrated for the DJI Phantom 2 quadrotor in three realistic scenarios.es_ES
Doihttps://doi.org/10.1109/icra.2016.7487285es_ES
ISBN978-146738026-3es_ES
URIhttps://riuat.uat.edu.mx/handle/123456789/6517
IdiomaInglés[20]es_ES
EditorialInstitute of Electrical and Electronics Engineers Inc.es_ES
RelaciónProceedings - IEEE International Conference on Robotics and Automationes_ES
URL relacionadohttps://doi.org/10.1109/icra.2016.7487285es_ES
DerechosAcceso restringido / Suscripción (Metadatos de producción científica)es_ES
Licenciahttp://purl.org/coar/access_right/c_16eces_ES
FuenteProceedings - IEEE International Conference on Robotics and Automation
TítuloMinimum-energy path generation for a quadrotor UAVes_ES
TipoPonenciaes_ES
ArbitradoHa sido Arbitradoes_ES
AutorMorbidi, Fabio
AutorCano, Roel
AutorLara, David
AutorMorbidi, Fabioes_ES
AutorCano, Roeles_ES
AutorLara, Davides_ES
InstituciónUniversidad Autónoma de Tamaulipas
InstituciónUniversidad Autónoma de Tamaulipases_ES
Rango de páginas1492-1498es_ES
URL relacionadahttps://doi.org/10.1109/icra.2016.7487285
Tipo de artículoIndexado
Tipo de artículoIndexadoes_ES
Volumen2016-Junees_ES

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