%0 Journal Article %A Dubov, Yury Borisovich %D 2013 %I Begell House %K inertia coupled maneuver, gyroscope torque, roll rate and yaw rate, angle of attack, sideslip angle %N 2 %P 245-253 %R 10.1615/TsAGISciJ.2013008114 %T ANALYSIS OF INTERACTION OF LONGITUDINAL AND LATERAL MOTION OF THE MANEUVERABLE AIRCRAFT WHEN REACHING HIGH ANGLE OF ATTACK %U https://www.dl.begellhouse.com/journals/58618e1439159b1f,5cadfcb91b5f9b0f,2a9af9e47a926e8d.html %V 44 %X The reasons for aircraft roll and yaw rate overshoot are analyzed when being piloted at large angles of attack. Approximate analytical expressions for estimation of the overshoot values are given. %8 2013-10-23