THE COMPUTER MODELS APPLING AT FLIGHT INFORMATION PROCESSING

Describing information processing using mathematical modeling and numerical methods is currently one of the most effective ways. Some flight parameters are not recorded explicitly by the onboard recorder, so there is a need to develop a methodology for obtaining these parameters from indirect data contained in the flight data. This article presents technique in order to obtain the required information contained in these data in an implicit form. A method of using the data of the flight recorder, which fixes the parameters of the aircraft movement is presented. An original way of combining computer models and flight data is proposed. The mathematical techniques used in the process of identification are described. The purpose of the work is to present simulation computational experiments and determine all the coefficients at different stages. The result is smoothing of errors. High accuracy is required for predictive calculations. For example, determining the takeoff distance. In this case, an analytical solution is applicable, or, if not available, an exact method based on identification data.

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Publication Details

Published
2024-10-14
DOI
https://doi.org/10.57033/tdtu.uz.309
Primary Topic
Advanced Control and Stabilization in Aerospace Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

THE COMPUTER MODELS APPLING AT FLIGHT INFORMATION PROCESSING

Ismail Ismailov, Jeyran Agamaliyeva
Advanced Control and Stabilization in Aerospace Systems
article

THE COMPUTER MODELS APPLING AT FLIGHT INFORMATION PROCESSING

Ismail Ismailov, Jeyran Agamaliyeva
article en

Abstract

Describing information processing using mathematical modeling and numerical methods is currently one of the most effective ways. Some flight parameters are not recorded explicitly by the onboard recorder, so there is a need to develop a methodology for obtaining these parameters from indirect data contained in the flight data. This article presents technique in order to obtain the required information contained in these data in an implicit form. A method of using the data of the flight recorder, which fixes the parameters of the aircraft movement is presented. An original way of combining computer models and flight data is proposed. The mathematical techniques used in the process of identification are described. The purpose of the work is to present simulation computational experiments and determine all the coefficients at different stages. The result is smoothing of errors. High accuracy is required for predictive calculations. For example, determining the takeoff distance. In this case, an analytical solution is applicable, or, if not available, an exact method based on identification data.

Openalex Percentile: Top 61%
Advanced Control and Stabilization in Aerospace Systems
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