Please use this identifier to cite or link to this item:Volltext verfügbar? / Dokumentlieferung
|Title:||Hybrid Aeronautical Propulsion: Control and Energy Management|
Monopoli, Vito G.
|Year of Publication:||2017|
|Publikation type:||Journal Article|
|Abstract:||In this paper, a control strategy for energy management of a parallel hybrid electric UAV (Unmanned Air Vehicle) powertrain is presented. A Simulink-based model of the system is first presented, consisting of an internal combustion engine, a gearbox (which includes a planetary gear and a continuously variable transmission), an electric motor (which can also work as a generator), an electric drive (Inveter) and a Li-Po battery pack. The proposed control strategy consists of a quasi-real-time iterative algorithm based on Dynamic Programming, which allows to optimize power management and torque-split of the powertrain with final state constraints on state variable. Aim of the study is to investigate new flight capabilities that derive from the use of a hybrid architecture, e.g., silent mode using only electric motor (useful for military and civil purpose), and the capacity of reducing fuel consumption. Simulation studies are performed, based on data of an existing UAV and a real flight mission.|
|DOI of the first publication:||10.1016/j.ifacol.2017.12.031|
|URL of the first publication:||https://www.sciencedirect.com/science/article/pii/S240589631733567X|
|Link to this record:||hdl:20.500.11880/28188|
|Date of registration:||24-Oct-2019|
|Faculty:||NT - Naturwissenschaftlich- Technische Fakultät|
|Department:||NT - Systems Engineering|
|Professorship:||NT - Prof. Dr. Stefan Seelecke|
|Collections:||UniBib – Die Universitätsbibliographie|
Files for this record:
There are no files associated with this item.
Items in SciDok are protected by copyright, with all rights reserved, unless otherwise indicated.