Endurance-Oriented Model Predictive Energy Management for a Proton Exchange Membrane Fuel Cell-Battery Hybrid Quadcopter Under Dynamic Mission Conditions

dc.contributor.authorKayaoglu, Murat
dc.contributor.authorUnal, Sencer
dc.contributor.authorBiyik, Hilal
dc.date.accessioned2026-09-08T07:11:43Z
dc.date.issued2026
dc.departmentFırat Üniveristesi
dc.description.abstractProton exchange membrane fuel cell-battery hybrid power systems provide an effective solution to overcome the limited endurance of battery-powered multirotor unmanned aerial vehicles. However, the highly transient power demands of quadcopter platforms, combined with balance-of-plant losses and operational constraints, create significant challenges for reliable energy management. This study proposes a degradation-aware stress-mitigation model predictive control-based energy management framework to maximize mission endurance under realistic conditions. A control-oriented, physics-consistent model is developed using manufacturer polarization data from a 500 W Aerostak proton exchange membrane fuel cell. The model captures polarization behavior, balance-of-plant loads, battery dynamics, and direct current-bus power balance. The model predictive control strategy optimally allocates power by maintaining direct current-bus stability, regulating battery state-of-charge within safe limits, and constraining fuel cell power ramp rates to mitigate degradation. High-fidelity simulations are conducted under stochastic wind disturbances and mission-dependent load profiles, including takeoff, climb, cruise, and maneuvering phases. The results show continuous power delivery without unmet load demand. The hybrid system achieves a flight endurance of 220-224 min, consuming a total of 89.99 g of hydrogen at an average rate of 0.398-0.412 g/min, indicating a notable reduction under the considered operating conditions. Additionally, long-term analysis indicates that over 97% of initial endurance is preserved after 100 cycles, demonstrating robustness against fuel cell aging. An analytical real-time feasibility assessment further indicates that the control-oriented formulation is compatible with the computational resources of typical unmanned aerial vehicle-class onboard processors, while the integration of adaptive and robust predictive control techniques is identified as a direction for future work.
dc.description.sponsorshipThis research received no external funding.
dc.identifier.doi10.3390/ma19122548
dc.identifier.issn1996-1944
dc.identifier.issue12
dc.identifier.pmid42355130
dc.identifier.scopus2-s2.0-105043021051
dc.identifier.scopusqualityQ1
dc.identifier.urihttps://doi.org/10.3390/ma19122548
dc.identifier.urihttps://hdl.handle.net/11508/65118
dc.identifier.volume19
dc.identifier.wosWOS:001803230700001
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.indekslendigikaynakPubMed
dc.language.isoen
dc.publisherMdpi
dc.relation.ispartofMaterials
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_WOS_20250903
dc.subjectProton Exchange Membrane Fuel Cell
dc.subjectHybrid Uav
dc.subjectEnergy Management Strategies
dc.subjectEndurance Optimization
dc.titleEndurance-Oriented Model Predictive Energy Management for a Proton Exchange Membrane Fuel Cell-Battery Hybrid Quadcopter Under Dynamic Mission Conditions
dc.typeArticle

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