Software System for Thrust Prediction and Preliminary Engineering Design of Aircraft Using Visual Recognition and Flight Parameters
Accurate estimation of engine thrust and overload is crucial for ensuring structural integrity and optimizing the aircraft’s life-cycle design. To address this issue, this study develops an integrated thrust and load prediction framework that combines vision-based flight maneuver recognition with an improved transformer-based deep learning model (YOLO), leveraging measured flight parameters. After maneuver recognition, the model achieves a mean absolute error of 1.86 and R2 of 0.97 in prediction. The framework is implemented via a Python-based software system with a MySQL database, supporting functionalities including thrust/load prediction, trajectory visualization, and performance evaluation. Comparative experiments demonstrate that the framework achieves an average maneuver recognition accuracy of 81.06%, outperforming the existing PLR-PIP and DTW methods. This approach provides high-precision and reliable thrust data as well as tool support for real-time thrust estimation, fatigue life assessment, and flight safety risk prevention.
Authors
- Zhiping Yin (ORCID: https://orcid.org/0000-0002-7567-0100)
- Yue Ma (ORCID: https://orcid.org/0000-0002-6107-4455)
- Mengchuang Zhang (ORCID: https://orcid.org/0000-0003-2456-5818)
- Shifeng Mao (ORCID: https://orcid.org/0000-0002-2370-1585)
- Juan Du (ORCID: https://orcid.org/0000-0001-8927-2667)
- Rui Wang (ORCID: https://orcid.org/0000-0002-4495-6405)
Institutions
- Aviation Industry Corporation of China (China) (CN)
- Northwestern Polytechnical University (CN)
- Craft Group (China) (CN)
Publication Details
- Journal
- Applied Sciences
- Published
- 2025-11-04
- DOI
- https://doi.org/10.3390/app152111770
- Primary Topic
- Advanced Aircraft Design and Technologies
- Type
- article
- Field-Weighted Citation Impact
- 0.00