The doi 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: 10.4121/8dc704cb-80b0-493d-9723-5ec25f2667c9

Tomaso De Ponti (2024): Test data of the Unified Actuator Nonlinear Dynamic Inversion controller for the Variable Skew Quad plane. Version 3. 4TU.ResearchData. dataset. https://doi.org/10.4121/8dc704cb-80b0-493d-9723-5ec25f2667c9.v3

Dataset

x choose version: version 2 - 2024-03-28 version 1 - 2024-03-07

• Aerospace Engineering
• Engineering

Actuator Nonlinear Dynamic Inversion, Error Controller, Incremental Nonlinear Dynamic Inversion, Reference Model, Variable Skew Quad Plane

CC BY-NC-SA 4.0

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Tomaso De Ponti

This dataset accompanies the paper titled "Unified Actuator Nonlinear Dynamic Inversion controller for the Variable Skew Quad Plane." It includes flight test data, simulation data, post-processing scripts, and derivations. The presented controller is demonstrated to be superior in tracking position and attitude trajectories compared to an Incremental Nonlinear Dynamic Inversion controller. The dataset contains simulation and real indoor testing data comparing the trajectory tracking performance of the two controllers.

• 2024-03-07 first online

• 2024-12-11 published, posted

4TU.ResearchData

Matlab, Simulink and PDF

TU Delft, Faculty of Aerospace Engineering, Department of Control & Simulation