THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SOME LATERAL CONTROL DERIVATIVES OF RECTANGULAR. WING

INVESTIGATION OF HELICOPTER STABILITY CONSIDERING THE EFFECT OF ITS HYDRAULIC SERVOACTUATOR AND AUTOPILOT

Flight Dynamics, Stability and Control of a Flexible Airplane

SOME ASPECTS OF AN EXPERIMENTAL INVESTIGATION ON COMPOSITE AEROBATIC AIRCRAFT STRUCTURE.

INVESTIGATION OF THE OPERATION OF AN ELECTROHYDRAULIC CONTROL SYSTEM OF A FLYING VEHICLE UNDER FAILURE CONDITIONS

Computational Aerodynamics Analysis of a Light Aircraft

MODELLING OF AN AIRCRAFT LONGITUDINAL CONTROL SYSTEM.

EFFECT OF AERODYNAMIC CROSS-COUPLING ON THE STABILITY OF A ROLLING AIRCRAFT

ANALYSIS OF A LIGHT AIRCRAFT RESPONSE TO GUST WIND BASED ON NONLINEAR MODEL

AN INVESTIGATION OF HELICOPTER FUSELAGE NORMAL MODES OF VIBRATION