Navigation and Control Conference : Approximation of 6DOF characteristics in 3DOF launch vehicle ascent simulations
INVESTIGATION OF THE APPLICABILITY OF THE FREE-WING PRINCIPLE TO LIGHT, GENERAL AVIATION AIRCRAFT by Ricburd F. Porter, Ross G.
NASA I Aeronautical Engineering Aer ering Aeronautical Engineerin igineerjng Aeronautical Engin Dal Engineering Aeronautical E n
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