Investigation of small-scale propellers under non-axial inflow conditions

M Cerny, C Breitsamter - Aerospace Science and Technology, 2020 - Elsevier
Small-scale propellers, especially those used on conventional multicopter configurations or
in the context of urban air mobility, may experience high inflow angles. In order to improve …

Adaptive incremental nonlinear dynamic inversion for attitude control of micro air vehicles

EJJ Smeur, Q Chu, GCHE De Croon - Journal of Guidance, Control …, 2016 - arc.aiaa.org
Incremental nonlinear dynamic inversion is a sensor-based control approach that promises
to provide high-performance nonlinear control without requiring a detailed model of the …

Ten questions concerning the use of drones in urban environments

S Watkins, J Burry, A Mohamed, M Marino… - Building and …, 2020 - Elsevier
The backdrop to the rapidly expanding use of drones is described, including development of
drone technology, followed by an overview of current civilian use, focusing on use in and …

System identification for propellers at high incidence angles

BM Simmons - Journal of Aircraft, 2021 - arc.aiaa.org
Propellers used for electric vertical takeoff and landing (eVTOL) aircraft propulsion systems
experience a wide range of aerodynamic conditions, including large incidence angles …

Choosing the best embedded processing platform for on-board UAV image processing

D Hulens, J Verbeke, T Goedemé - … 2015, Berlin, Germany, March 11–14 …, 2016 - Springer
Nowadays, complex image processing algorithms are a necessity to make UAVs more
autonomous. Currently, the processing of images of the on-board camera is often performed …

Quadrotor control in a wind field

NK Tran, E Bulka, M Nahon - 2015 International Conference on …, 2015 - ieeexplore.ieee.org
This paper investigates the ability of a quadrotor to maneuver in a wind field. A dynamic
model of a quadrotor is presented to model its motion. The quadrotor model includes a wind …

Experimental and numerical study of micro-aerial-vehicle propeller performance in oblique flow

B Theys, G Dimitriadis, P Hendrick, J De Schutter - Journal of aircraft, 2017 - arc.aiaa.org
This paper presents the modeling of the performance of small propellers used for vertical
takeoff and landing micro aerial vehicles operating at low Reynolds numbers and in oblique …

Experimental Analysis of a Small‐Scale Rotor at Various Inflow Angles

A Kolaei, D Barcelos… - International Journal of …, 2018 - Wiley Online Library
The performance characteristics of a rotor that is typically used for small unmanned aircraft
were analyzed in a series of wind‐tunnel experiments. Wind‐tunnel measurements were …

Experimental investigation of UAV rotor aeroacoustics and aerodynamics with computational cross-validation

AA Kostek, F Lößle, R Wickersheim, M Keßler… - CEAS Aeronautical …, 2024 - Springer
The study provided a base of comparison of known computational techniques with different
fidelity levels for performance and noise prediction of a single, fixed-pitch UAV rotor …

A propeller model for general forward flight conditions

W Khan, M Nahon - International Journal of Intelligent Unmanned …, 2015 - emerald.com
Purpose–The purpose of this paper is to develop a physics-based model for UAV propellers
that is capable of predicting all aerodynamic forces and moments in any general forward …