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Author

Vasif Karimli

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Open access Sep 2026

Improving the aerodynamic stability and controllability of aircraft, considering the speed of sound and maneuvering oscillations under disturbing atmospheric conditions

An aircraft's aerodynamic stability and controllability in pitch, roll, and yaw are determined by its flight performance and actual flight conditions. Traditional stability augmentation systems based on gyroscopic and inertial feedback are activated only after a disturbance has been applied, so the aircraft first acqui...

Toghrul Karimli, A. Mammadov, R. Guliyev et al. · 0 citations

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