Abstract
In order to study the safety of civil aircraft during approach and landing, models of mean wind, turbulence and wind shear were established. The mean wind model is obtained by fitting the probability statistics of the scalar wind speed and wind direction of the mean wind. Based on Von Karman model, the statistical characteristics of turbulence model are obtained by passing Gaussian random white noise through filter. According to the relationship between turbulence scale, turbulence intensity and ground height stipulated by airworthiness regulations, the characteristics of low altitude turbulence are analyzed, and the feasibility of the turbulence model in the approach landing stage of civil aircraft is verified. The wind shear model is obtained based on the principle of aerodynamics, and the characteristics of the low-altitude microburst are analyzed. Simulation results show that the model has reached the requirements of airworthiness regulations. Finally, according to the simulation results, the feasibility and accuracy of the model in airworthiness verification of the automatic landing system of civil aircraft are studied.
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References
Boeing. Statistical summary of commercial jet airplane accidents (2017). https://skybrary.aero
Zhang, H., Wu, J.: Research on typical flight accidents of civil aircraft under extreme climatic conditions. Technol. Innov. 132–134 (2019)
International civil aviation organization. Annex 10 to the convention on international civil aviation: aeronautical telecommunications, volume I - radio navigation aids (2018). https://www.icao.int/Pages/default.aspx
European aviation safety agency. CS-AWO-2003, certification specification for all weather operations (2003). https://www.easa.europa.eu
Shakarian, A.: Application of monte-carlo techniques to the 757/767 auto-land dispersion analysis by simulation. AIAA (1983)
Civil aviation administration of China. CCAR-25-R4, Airworthiness standards for transport aircraft (2016). http://www.caac.gov.cn/index.html
Federal aviation administration. AC120–28D, Criteria for approval of category III weather minima for takeoff, landing, and rollout (1999). https://www.faa.gov/regulations_polic-ies/advisory_circulars
Gao, Z., Gu, H.: Research on modeling of flight dynamics for large aircraft in complex atmospheric disturbance. J. Syst. Simul. 21(17), 5556–5561 (2009)
Chen, J., Wang, L., Li, Z., Wang, Q.: Application of microburst wind field model in ballistic simulation. J. Ballistics 31(04), 33–38 (2019)
Pan, X.: Fluid Mechanics and Heat Transfer, 1st edn. Jiangxi Universities and Colleges Press, Location (2019)
Federal aviation administration. AC120–41, Criteria for operational approval of airborne wind shear alerting and flight guidance systems (1983). https://www.faa.gov/regula-tions_policies/advisory_circulars
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Yu, Q., Li, L., Li, D., Xu, H., Zhang, C. (2023). Simulation of Atmospheric Disturbance During Approaching and Landing of Civil Aircraft. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_593
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DOI: https://doi.org/10.1007/978-981-19-6613-2_593
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