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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Published

2010-11-12

How to Cite

[1]
A. Y. Volovyk, Y. M. Volovyk, V. V. Zahorskyi, and M. A. Shutylo, “Optimal evaluation of angular coordinates of airplane during landing”, Вісник ВПІ, no. 5, pp. 20–26, Nov. 2010.

Issue

No 5 (2007)

Section

Automation and information-measuring equipment

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