| Jorge González-García |
Department of Aerospace Engineering, Universidad Carlos III de Madrid, Avenida de la Universidad 30, 28911 Leganés (Madrid), Spain. | | Francisco DeLosRíos-Navarrete |
Department of Aerospace Engineering, Universidad Carlos III de Madrid, Avenida de la Universidad 30, 28911 Leganés (Madrid), Spain. CT Ingenieros A.A.I. S.L. Avenida Leonardo Da Vinci 22, 28050 Getafe (Madrid), Spain. | | David Santos-Martín |
Department of Electrical Engineering, Universidad Carlos III de Madrid, Avenida de la Universidad 30, 28911 Leganés (Madrid), Spain. | | Gonzalo Sánchez-Arriaga |
Department of Aerospace Engineering, Universidad Carlos III de Madrid, Avenida de la Universidad 30, 28911 Leganés (Madrid), Spain. |
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| Abstract:
Airborne Wind Energy (AWE) systems require reliable control architectures to achieve autonomous and repeatable flight under realistic operating conditions. To support controller development while reducing the cost and risk associated with field experiments, a Hardware-in-the-Loop (HIL) platform for closed-loop validation of external flight controllers is presented. The proposed setup combines a high-fidelity kite dynamics model executed in real time, with a Ground Control Unit (GCU), wireless communication modules, and physical actuators. The platform is assessed in terms of computational performance, communication latency, and path-following capability. The results show that the proposed HIL setup sustains real-time operation and enables stable closed-loop tracking of ten figure-eight trajectories, providing a practical intermediate validation stage between offline simulation and flight testing.
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