Data and Code for Unmanned Aerial Vehicles airspeed estimation using propeller feedback.

DOI:10.4121/8bcecbac-5478-4595-b629-4378feac6dcb.v1
The DOI displayed above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
DOI: 10.4121/8bcecbac-5478-4595-b629-4378feac6dcb

Datacite citation style

Ntouros, Evangelos; Kelley, Pavel; Smeur, Ewoud (2025): Data and Code for Unmanned Aerial Vehicles airspeed estimation using propeller feedback. Version 1. 4TU.ResearchData. software. https://doi.org/10.4121/8bcecbac-5478-4595-b629-4378feac6dcb.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Software

This repository contains MATLAB scripts to derive and validate an airspeed model for fixed-wing Unmanned Aerial Vehicles (UAVs) using solely propeller power and rotational speed data. The model can be used to replace Pitot-tube-based airspeed sensors, or contribute to redundancy in airspeed estimation. It does not require knowledge of the vehicle’s dynamic model and is computationally lightweight. It leverages power and rotational speed feedback, which is readily available from modern Electronic Speed Controllers (ESCs), thereby enabling seamless integration with existing systems and off-the-shelf components.

History

  • 2025-10-07 first online, published, posted

Publisher

4TU.ResearchData

Format

.m, .mat, .dat, .eps, .fig, .jl, .png

Associated peer-reviewed publication

Airspeed estimation for UAVs using only propeller feedback

Organizations

TU Delft, Faculty of Aerospace Engineering, Department of Control and Operations, Section Control & Simulation

DATA

To access the source code, use the following command:

git clone https://data.4tu.nl/v3/datasets/37eb50b9-265a-472a-9488-ed6719d5c318.git "propeller_airspeed_sensor"

Or download the latest commit as a ZIP.

Files (1)

  • 8,994,732 bytesMD5:e02406912dffc42cfac5838ae08ff721data.tar.xz