Abstract
This paper presents the modeling and control of an interleaved bidirectional DC–DC converter responsible for the interconnection of a battery pack to an aircraft turbo-electric propulsion system. Proposed model has been developed based on state-space averaging and small-signal linearization techniques. Design of current and voltage controllers established to perform the proposed battery management approach is described. Processor-in-the-loop simulations, implemented using microcontroller and Simulink, have been conducted for case studies analysis and validation of proposed strategy, where hybrid and fully electric aircraft operation modes have been evaluated.
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Acknowledgements
An early version of paper was presented at XXIII Congresso Brasileiro de Automática (CBA 2020). Authors thank to the funding agencies CAPES, CNPq, and FAPEMIG, as well as UFJF and Embraer, for supporting this work. Also, they would like to thank Eng. Otávio Gomes for his technical contribution.
Funding
Funding was provided by Fundação de Amparo à Pesquisa do Estado de Minas Gerais (Grant No. FAPEMIG/Embraer APQ-03593-17, FAPEMIG APQ-01378-16) and Conselho Nacional de Desenvolvimento Científico e Tecnológico (Grant No. CNPq 432307-2016-8).
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Bastos, M.E.S., Nascimento, S.O., Torres, V.C.S. et al. Control Strategy for an Interleaved Bidirectional DC–DC Converter Applied to Battery Management in a Hybrid Aircraft Propulsion System. J Control Autom Electr Syst 33, 965–973 (2022). https://doi.org/10.1007/s40313-021-00883-x
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DOI: https://doi.org/10.1007/s40313-021-00883-x