Back to Search
Start Over
Modelling and Hovering Stabilisation of a Free-Rotating Wing UAV
- Source :
- 2024 International Conference on Unmanned Aircraft Systems (ICUAS), Jun 2024, La Can{\'e}e (Crete), Greece. pp.779-785
- Publication Year :
- 2024
-
Abstract
- We propose a multibody model of a freewing UAV. This model allows obtaining simulations of the UAV's behaviour and, in the future, to design a control law stabilising the entire flight envelope (hovering and forward flight). We also describe the realisation of a prototype and a comparison of possible methods for estimating the UAV's states. With this prototype, we report on experimental hovering flights with a non-linear incremental dynamic inversion controller to stabilise the wing and a proportional derivative controller for the fuselage stabilization.
- Subjects :
- Computer Science - Robotics
Subjects
Details
- Database :
- arXiv
- Journal :
- 2024 International Conference on Unmanned Aircraft Systems (ICUAS), Jun 2024, La Can{\'e}e (Crete), Greece. pp.779-785
- Publication Type :
- Report
- Accession number :
- edsarx.2406.17313
- Document Type :
- Working Paper
- Full Text :
- https://doi.org/10.1109/ICUAS60882.2024.10556832