Modeling and control of an overactuated aerial vehicle with four tiltable quadrotors attached by means of passive universal joints

Imanol Iriarte, Erlantz Otaola, David Culla, Inaki Iglesias, Joseba Lasa, Basilio Sierra

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

3 Citas (Scopus)
17 Descargas (Pure)

Resumen

We present a novel overactuated aerial vehicle based on four quadrotors connected to an airframe by means of passive universal joints. The proposed architecture allows to independently control the six degrees of freedom of the airframe without having fixed propellers at inefficient configurations or making use of dedicated rotor tilting actuators. After deriving the dynamic equations that describe its motion, we propose a linear control strategy that is able to successfully decouple rotation and translation, relying exclusively on on-board sensors. A prototype is built and preliminary experimental results demonstrate that the concept is feasible.Video: https://youtu.be/9ASP3FyhCJw.
Idioma originalInglés
Título de la publicación alojadaunknown
EditorialIEEE
Páginas1748-1756
Número de páginas9
ISBN (versión digital)978-1-7281-4278-4, 9781728142777
ISBN (versión impresa)978-1-7281-4279-1
DOI
EstadoPublicada - oct 2020
Evento2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020 - Athens, Grecia
Duración: 1 sept 20204 sept 2020

Serie de la publicación

Nombre2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

Conferencia

Conferencia2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
País/TerritorioGrecia
CiudadAthens
Período1/09/204/09/20

Palabras clave

  • Propellers
  • Torque
  • Rotors
  • Actuators
  • Aerodynamics
  • Complexity theory

Project and Funding Information

  • Funding Info
  • This research was supported by the ELKARTEK 2018 program of the Basque Government, grant agreement No. KK-2018/00082.

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