Endurance-Oriented Model Predictive Energy Management for a Proton Exchange Membrane Fuel Cell-Battery Hybrid Quadcopter Under Dynamic Mission Conditions
| dc.contributor.author | Kayaoglu, Murat | |
| dc.contributor.author | Unal, Sencer | |
| dc.contributor.author | Biyik, Hilal | |
| dc.date.accessioned | 2026-09-08T07:11:43Z | |
| dc.date.issued | 2026 | |
| dc.department | Fırat Üniveristesi | |
| dc.description.abstract | Proton 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.sponsorship | This research received no external funding. | |
| dc.identifier.doi | 10.3390/ma19122548 | |
| dc.identifier.issn | 1996-1944 | |
| dc.identifier.issue | 12 | |
| dc.identifier.pmid | 42355130 | |
| dc.identifier.scopus | 2-s2.0-105043021051 | |
| dc.identifier.scopusquality | Q1 | |
| dc.identifier.uri | https://doi.org/10.3390/ma19122548 | |
| dc.identifier.uri | https://hdl.handle.net/11508/65118 | |
| dc.identifier.volume | 19 | |
| dc.identifier.wos | WOS:001803230700001 | |
| dc.identifier.wosquality | Q2 | |
| dc.indekslendigikaynak | Web of Science | |
| dc.indekslendigikaynak | Scopus | |
| dc.indekslendigikaynak | PubMed | |
| dc.language.iso | en | |
| dc.publisher | Mdpi | |
| dc.relation.ispartof | Materials | |
| dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | |
| dc.rights | info:eu-repo/semantics/openAccess | |
| dc.snmz | KA_WOS_20250903 | |
| dc.subject | Proton Exchange Membrane Fuel Cell | |
| dc.subject | Hybrid Uav | |
| dc.subject | Energy Management Strategies | |
| dc.subject | Endurance Optimization | |
| dc.title | Endurance-Oriented Model Predictive Energy Management for a Proton Exchange Membrane Fuel Cell-Battery Hybrid Quadcopter Under Dynamic Mission Conditions | |
| dc.type | Article |







