Design, control, and visual navigation of the DelftaCopter VTOL tail-sitter UAV

Journal Article (2018)
Author(s)

Christophe De Wagter (TU Delft - Control & Simulation)

Rick Ruijsink (TU Delft - Control & Simulation)

Ewoud Smeur (TU Delft - Control & Simulation)

K.G. van Hecke (TU Delft - Control & Simulation)

F. van Tienen (TU Delft - Control & Simulation)

E. van der Horst (TU Delft - Control & Simulation)

B. D. W. Remes (TU Delft - Control & Simulation)

Research Group
Control & Simulation
Copyright
© 2018 C. de Wagter, Rick Ruisink, E.J.J. Smeur, K.G. van Hecke, F. van Tienen, E. van der Horst, B.D.W. Remes
DOI related publication
https://doi.org/10.1002/rob.21789
More Info
expand_more
Publication Year
2018
Language
English
Copyright
© 2018 C. de Wagter, Rick Ruisink, E.J.J. Smeur, K.G. van Hecke, F. van Tienen, E. van der Horst, B.D.W. Remes
Research Group
Control & Simulation
Issue number
6
Volume number
35
Pages (from-to)
937-960
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

To participate in the Outback Medical Express UAV Challenge 2016, a vehicle was designed and tested that can autonomously hover precisely, takeoff and land vertically, fly fast forward efficiently, and use computer vision to locate a person and a suitable landing location. The vehicle is a novel hybrid tail‐sitter combining a delta‐shaped biplane fixed‐wing and a conventional helicopter rotor. The rotor and wing are mounted perpendicularly to each other,and the entire vehicle pitches down to transition from hover to fast forward flight where the rotor serves as propulsion. To deliver sufficient thrust in hover while still being efficient in fast forward flight, a custom rotor system was designed. The theoretical design was validated with energy measurements, wind tunnel tests, and application in real‐world missions. A rotor‐head and corresponding control algorithm were developed to allow transitioning flight with the nonconventional rotor dynamics that are caused by the fuselage rotor interaction. Dedicated electronics were designed that meet vehicle needs and comply with regulations to allow safe flight beyond visual line of sight. Vision‐based search and guidance algorithms running on a stereo‐vision fish‐eye camera were developed and tested to locate a person in cluttered terrain never seen before. Flight tests and a competition participation illustrate the applicability of the DelftaCopter concept.