The pursuit for cleaner aviation pushes research in hybrid-electric aircraft, which are far more complex systems than conventional airplanes. In this respect, the ODE4HERA European project aims to accelerate the development of such systems with the implementation of a solution-neutral Open Digital Platform, driving the design from top level requirements to virtual verification and validation. In this respect, the authors developed and integrated a flight dynamics module in a co-simulation environment aiming at the performance verification of the reference hybrid-electric aircraft through flight simulation. The implementation of a point mass model was sufficiently accurate to comply with the preliminary objectives of the project, paving the way for a higher-fidelity and more complex flight dynamics and control systems.
Development and Integration of a Flight Dynamics Module into the ODE4HERA Open Digital Platform / Ciliberti, D., De Marco, A., Nicolosi, F.. - In: ENGINEERING PROCEEDINGS. - ISSN 2673-4591. - 133:1(2026). (15th EASN International Conference Madrid (Spagna) 14-17 ottobre 2025) [10.3390/engproc2026133063].
Development and Integration of a Flight Dynamics Module into the ODE4HERA Open Digital Platform
Danilo Ciliberti
Primo
Writing – Original Draft Preparation
;Agostino De MarcoSecondo
Supervision
;Fabrizio NicolosiUltimo
Project Administration
2026
Abstract
The pursuit for cleaner aviation pushes research in hybrid-electric aircraft, which are far more complex systems than conventional airplanes. In this respect, the ODE4HERA European project aims to accelerate the development of such systems with the implementation of a solution-neutral Open Digital Platform, driving the design from top level requirements to virtual verification and validation. In this respect, the authors developed and integrated a flight dynamics module in a co-simulation environment aiming at the performance verification of the reference hybrid-electric aircraft through flight simulation. The implementation of a point mass model was sufficiently accurate to comply with the preliminary objectives of the project, paving the way for a higher-fidelity and more complex flight dynamics and control systems.| File | Dimensione | Formato | |
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engproc-133-00063-v2.pdf
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