Methods of a Priori Statistical Analysis of Disturbed Motion of Aircraft in Turbulent Environments
- 作者: Ermilov A.S.1, Saltykova O.A.1
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隶属关系:
- RUDN University
- 期: 卷 25, 编号 4 (2024)
- 页面: 348-356
- 栏目: Articles
- URL: https://journals.rcsi.science/2312-8143/article/view/327552
- DOI: https://doi.org/10.22363/2312-8143-2024-25-4-348-356
- EDN: https://elibrary.ru/EWJUVW
- ID: 327552
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详细
The article discusses the methods of a priori statistical analysis used for predicting perturbed motion of aircraft in turbulent environments. Theoretical approaches such as the comparative method and mathematical modeling method are used to analyze the a priori analysis methods. The paper also utilizes statistical methods to evaluate the effectiveness of stochastic models to account for random perturbations caused by turbulence. Special attention is paid to the use of Bayesian analysis, maximum likelihood method and Monte Carlo method applied for probabilistic prediction of the aircraft trajectory. The presented models are illustrated with formulas that describe the dynamics of vehicle motion in turbulent conditions, including equations of motion based on Newton’s and Euler’s laws. The parameters that determine the dynamics of the perturbed motion of the aircraft in a turbulent environment, such as linear and angular velocities, turbulence intensity, aerodynamic forces, moments of inertia and meteorological conditions, are studied to evaluate the correctness of the calculations. This allows the effects of turbulence on the control and flight trajectory of the aircraft to be taken into account. The results of the study demonstrate the high accuracy of the proposed methods in predicting aircraft motion deviations and emphasize the importance of further development of computational approaches to integrate these methods into real-time control systems, especially for application in conditions of uncertainty and complex external influences. Further research could focus on improving the adaptability of models for different types of aircrafts, taking into account the optimization of computational methods to reduce computational complexity. This will make it possible to improve the efficiency of forecasts in a shorter time and reduce resource costs.
作者简介
Alexander Ermilov
RUDN University
Email: eemilov-sasha@yandex.ru
ORCID iD: 0009-0007-4549-172X
Postgraduate student of the Department of Mechanics and Control Processes, Academy of Engineering
Moscow, RussiaOlga Saltykova
RUDN University
编辑信件的主要联系方式.
Email: saltykova-oa@rudn.ru
ORCID iD: 0000-0002-3880-6662
SPIN 代码: 3969-6707
Cand. Sc. (Physics and Mathematics), Associate Professor of the Department of Mechanics and Control Processes, Academy of Engineering
Moscow, Russia参考
- Rassadin AA, Ryakhovsky AV. Modeling turbulent flow: a case study of wing profile streamlining. Advances in Cybernetics. 2024;5(2):64-74. (In Russ). https://doi.org/10.12345/jcyb.ru/issue5/64-74
- Kurnyshev DA, Mitin TA, Nyrkov DD. The problem of the stability of the disturbed and undisturbed motionof the aircraft. Modern Scientific Research: Current Issues, Achievements, and Innovations. Collection of articles of the XXXIV International Scientific and Practical Conference. Penza, August 15, 2023. 2023:22-27. (In Russ.) EDN: XRTCHK
- Raol JR, Singh J. Flight mechanics modeling and analysis. CRC Press; 2023.
- Kozhevnikov YuV, Shibanov GP. Optimum average of high-speed to describe of aircraft by the flying-tests. Mechatronics, Automation, Control. 2023;24(9):489-495. (In Russ). https://doi.org/10.31857/S0234-202310050
- Sirois J, Desjardins S, Peter G. Vortex-breakdown efficiency of planar regular grid structures - towards the development of design guidelines. Fluids. 2024;9(2):43. https://doi.org/10.3390/fluids9020043
- Kreerenko SS, Kreerenko OD. Parametric identi-fication of aerodynamic characteristics of a transport category aircraft using recurrent semi-empirical neural networks in the tensorflow environment. Mathematical modeling and computational methods. 2024;43(3):81-99. (In Russ.) https://doi.org/10.18698/2309-3684-2024-3-8199
- Astakhov SA, Ivanov VP, Sergeev IA. Aerody-namic interaction simulation during track testing of aircraft products. PNRPU Aerospace Engineering Bulletin. 2023;(72):5-20. (In Russ.) https://doi.org/10.15593/2224-9982/2023.72.01
- Kong Y, Mahadevan S. Identifying Anomalous Behavior in Aircraft Landing Trajectory Using a Bayesian Autoencoder. J Aerosp Inf Syst. 2024;21(1):19-27. https://doi.org/10.2514/1.J062834
- Bayat S, Amiri R. Advances in UAV-Assisted Localization: Joint Source and UAV Parameter Estimation. IEEE Trans Veh Technol. 2023;72(11):14268-78. https://doi.org/10.1109/TVT.2023.3190744
- Fedulov VA, Bykov NV, Baskakov VD. Estimat-ing of the effectiveness of the weapon system against of small unmanned aerial vehicles by computer simulation. Systems of Control, Communication and Security. 2023;(4):63-104. (In Russ.) https://doi.org/10.24412/2410-9916-2023-4-63-104
- An Z, Wang Y, Zhang Q. Learning spatial regu-larization correlation filters with the Hilbert-Schmidt independence criterion in RKHS for UAV tracking. IEEE Trans Instrum Meas. 2023;72:1-12. https://doi.org/10.1109/TIM.2023.3256114
- Israfilov A. Contemporary challenges in cyber-security of unmanned aerial systems. Universum: Technical Sciences. 2024;119(2):19-21. (In Russ.) EDN: SOIKHN
- Soldatov AS, Soldatov ES, Bogomolov AV. Tech-nological platform for digital twin synthesis of an aircraft based on cyber-physical systems technology. Large-Scale Systems Management (MLSD’2023): Proceedings of the Sixteenth Conference. Moscow, September 26-28, 2023, 2023:1092-1099. (In Russ.) https://doi.org/10.25728/mlsd.2023.1092
- Qiao W, Wu S. The Modeling and Simulation of Turbulence for Civil Aircraft Compliance Verification Test. J Phys Conf Ser. IOP Publishing. 2023;2658(1):012056. https://doi.org/10.1088/1742-6596/2658/1/012056
- Mohamed A, Cai W, Zhang R. Gusts encountered by flying vehicles in proximity to buildings. Drones. 2023;7(1):22. https://doi.org/10.3390/drones7010022
- Yoshimura R, Ishikawa S, Tanaka T, Nakamura Y. Clear air turbulence resolved by numerical weather pre-diction model validated by onboard and virtual flight data. Geophys Res Lett. 2023; 50(12):e2022GL101286. https://doi.org/10.1029/2022GL101286
- Jiang W, Gao L, Zhang X. An Investigation of Sudden Plunging Motion Mechanisms for Transport Aircraft during Severe Clear-Air Turbulence Encounter. J Aerosp Eng. 2023;36(3):04023011. https://doi.org/10.1061/(ASCE)AS.1943-5525.0001533
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