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Analytical and numerical linearization of the flight vehicle nonlinear dynamic model in the presence of wind
(ХАИ, 2017)
In this paper, nonlinear mathematical dynamic model for standard unmanned aerial vehicle, Aerosonde was
developed at low velocities in the presence of wind and then its linearized model was derived using numerical
and ...
Design of the robust PID control for uncertain nonlinear model of the UAV using artificial gain and time-delay model
(ХАІ, 2017)
Estimations of the flight vehicles aerodynamic coefficients through the theoretical, numerical, wind tunnel and flight-test methods have always errors and uncertainties. Nonlinear dynamics of the unmanned aerial vehicle ...