Automation and information-measuring equipment
Optimal evaluation of angular coordinates of airplane during landing
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.
How to Cite
[1]
“Optimal evaluation of angular coordinates of airplane during landing”, Вісник ВПІ, no. 5, pp. 20–26, Nov. 2010, Accessed: Oct. 29, 2026. Available: https://visnyk.vntu.edu.ua/index.php/visnyk/article/view/498
