This paper introduces a freeware open-source software ecosystem to design, tune, and test control systems for autonomous vertical take-off and landing (VTOL) multi-rotor uncrewed aerial vehicles (UAVs) such as quadcopters and quad-biplanes. This environment comprises C++-coded flight stacks with a suite of control systems, a high-fidelity simulator that allows model-in-the-loop and hardware-in-the-loop tests, computer-aided design (CAD) models of UAVs, and a website for a broad overview of this project. This ecosystem aims to serve as a common platform for the aerospace control community and ease comparative analyses for control design techniques produced by multiple research groups.
An Open-Source Framework to Design, Tune, and Fly Nonlinear Control Systems for Autonomous UAVs / Gramuglia, Mattia; Mugundan Kumar, Giri; Orlando, Giorgio A.; L'Afflitto, Andrea. - (2025). ( 2025 AIAA SciTech Forum Orlando, FL (USA) 6-10 January 2025) [10.2514/6.2025-2798].
An Open-Source Framework to Design, Tune, and Fly Nonlinear Control Systems for Autonomous UAVs
Giorgio A. Orlando;
2025
Abstract
This paper introduces a freeware open-source software ecosystem to design, tune, and test control systems for autonomous vertical take-off and landing (VTOL) multi-rotor uncrewed aerial vehicles (UAVs) such as quadcopters and quad-biplanes. This environment comprises C++-coded flight stacks with a suite of control systems, a high-fidelity simulator that allows model-in-the-loop and hardware-in-the-loop tests, computer-aided design (CAD) models of UAVs, and a website for a broad overview of this project. This ecosystem aims to serve as a common platform for the aerospace control community and ease comparative analyses for control design techniques produced by multiple research groups.| File | Dimensione | Formato | |
|---|---|---|---|
|
LAfflitto_Control_System_AIAA_Conference.pdf
accesso aperto
Tipologia:
2. Post-print / Author's Accepted Manuscript
Licenza:
Pubblico - Tutti i diritti riservati
Dimensione
605 kB
Formato
Adobe PDF
|
605 kB | Adobe PDF | Visualizza/Apri |
Pubblicazioni consigliate
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
https://hdl.handle.net/11583/2999420
