Please use this identifier to cite or link to this item: doi:10.22028/D291-29782
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Title: Hybrid Aeronautical Propulsion: Control and Energy Management
Author(s): Bongermino, Elisabetta
Tomaselli, Michele
Monopoli, Vito G.
Rizzello, Gianluca
Cupertino, Francesco
Naso, David
Language: English
Title: IFAC-PapersOnLine
Volume: 50
Issue: 2
Startpage: 169
Endpage: 174
Publisher/Platform: Elsevier
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
http://dx.doi.org/10.22028/D291-29782
ISSN: 2405-8963
1474-6670
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

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