A Next-Generation Hybrid Approach for Data-Driven Fuel-Efficient Flight Control of Commercial Aircraft
| dc.contributor.author | Ucar, Ukbe Usame | |
| dc.contributor.author | Kuzu, Zulfu | |
| dc.contributor.author | Aygun, Hakan | |
| dc.date.accessioned | 2026-08-12T17:28:43Z | |
| dc.date.issued | 2026 | |
| dc.department | Fırat Üniversitesi | |
| dc.description.abstract | In this study, a novel hybrid optimization approach is proposed to minimize the fuel consumption of commercial aircraft by taking flight-related and meteorological constraints into account during the cruise phase. The new method, the Decision Tree-Robust Multiple Regression-Harris Hawks Optimization Algorithm (DRHA), incorporates data segmentation based on decision trees, modeling of robust multiple regression, and the Harris Hawks optimization algorithm. In this context, a PID speed controller for a Boeing 737-800 aircraft was developed by employing a Software-in-the-Loop (SIL) framework that establishes real-time data exchange between MATLAB/Simulink and the FAA-approved X-Plane flight simulator. Within this framework, a simulation-based fuel consumption dataset was obtained from 1032 different scenarios encompassing various combinations of altitude, speed, aircraft weight, wind speed, and wind direction, thus aiming to reflect a wide range of realistic flight operating conditions. According to comparative analysis outcomes, the proposed DRHA approach significantly outperformed conventional statistical and machine learning-based methods in modeling fuel consumption equations. Namely, a mean absolute error (MAE) and R2 value are achieved with values of 1.24 and 0.90, respectively. Moreover, PID controller parameters are optimized under varying conditions thanks to the DRHA method, yielding between 0.07% and 5.33% fuel savings compared to manually tuned controllers. Tests performed under different altitudes, aircraft weights, and wind conditions confirm the algorithm's robustness and adaptability. The proposed method is anticipated to offer scalable and adaptable solutions for various types of aircraft and real-time control systems. | |
| dc.description.sponsorship | Firat University Research Fund [SHY.25.10] | |
| dc.description.sponsorship | Firat University Research Fund (SHY.25.10). | |
| dc.identifier.doi | 10.3390/aerospace13030289 | |
| dc.identifier.issn | 2226-4310 | |
| dc.identifier.issue | 3 | |
| dc.identifier.scopus | 2-s2.0-105034380987 | |
| dc.identifier.scopusquality | Q2 | |
| dc.identifier.uri | https://doi.org/10.3390/aerospace13030289 | |
| dc.identifier.uri | https://hdl.handle.net/11508/55414 | |
| dc.identifier.volume | 13 | |
| dc.identifier.wos | WOS:001725027700001 | |
| dc.identifier.wosquality | Q2 | |
| dc.indekslendigikaynak | Web of Science | |
| dc.indekslendigikaynak | Scopus | |
| dc.language.iso | en | |
| dc.publisher | Mdpi | |
| dc.relation.ispartof | Aerospace | |
| dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | |
| dc.rights | info:eu-repo/semantics/openAccess | |
| dc.snmz | KA_WoS_20260511 | |
| dc.subject | aircraft | |
| dc.subject | fuel consumption | |
| dc.subject | PID controller | |
| dc.subject | metaheuristic algorithm | |
| dc.title | A Next-Generation Hybrid Approach for Data-Driven Fuel-Efficient Flight Control of Commercial Aircraft | |
| dc.type | Article |







