Automation and information-measuring equipment

Optimal evaluation of angular coordinates of airplane during landing

Authors

A. Yu. Volovyk
Yu. M. Volovyk
V. V. Zahorskyi
M. A. Shutylo

Keywords

landing system kalman filter statistic modeling

Abstract

Mathematical model of airplane position angular dynamics variation during landing has been offered. Adequacy of the model is confirmed by the method of statistic modeling.
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How to Cite

[1]
“Optimal evaluation of angular coordinates of airplane during landing”, Вісник ВПІ, no. 5, pp. 20–26, Nov. 2010, Accessed: Oct. 05, 2026. Available: https://visnyk.vntu.edu.ua/index.php/visnyk/article/view/498

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