Aircraft Position Prediction during the Crosswind Approach

Testing the impact of the drag coefficient on an F16 aircraft model, depending on the angle of attack was performed. First, a navigation model was introduced describing the preliminary and computational assumptions of the model. The final part of the present paper contains the relationships between...

Full description

Bibliographic Details
Main Authors: Marek Grzegorzewski, Jerzy Biały
Format: Article
Language:English
Published: University of Žilina 2022-01-01
Series:Communications
Subjects:
Online Access:https://komunikacie.uniza.sk/artkey/csl-202201-0004_aircraft-position-prediction-during-the-crosswind-approach.php