ESTIMATION OF THE LATERAL AERODYNAMIC COEFFICIENTS FOR SKYWALKER X8 FLYING WING FROM REAL FLIGHT-TEST DATA

ESTIMATION OF THE LATERAL AERODYNAMIC COEFFICIENTS FOR SKYWALKER X8 FLYING WING FROM REAL FLIGHT-TEST DATA

Stability and control derivatives of Skywalker X8 flying wing from flight-test data are estimated by using the combination of the output error and least square methods in the presence of the wind. Data is collected from closed loop flight tests with a proportional-integral-derivative (PID) controlle...

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Bibliographic Details
Main Authors: Rahman Mohammadi Farhadi, Vyacheslav Kortunov, Andrii Molchanov, Tatiana Solianyk
Format: Article
Language:English
Published: CTU Central Library 2018-04-01
Series:Acta Polytechnica
Subjects:
flight system identification
aerodynamic coefficient estimation
data co-linearity
least square method
output error method
Online Access:https://ojs.cvut.cz/ojs/index.php/ap/article/view/4685

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https://ojs.cvut.cz/ojs/index.php/ap/article/view/4685

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