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