05.2 - Flight Dynamics and Control (UAV related)
A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE
Y.B. Been¹, Y.J. Kang¹, S.J. Shin¹; ¹Seoul National Univ., South Korea
A new solution method for six degree of freedom flight dynamics simulation of a high aspect ratio wing vehicle is introduced in this paper. And a simulation program is also constructed, which offers loads distribution on a complete vehicle and prediction of flight paths and attitudes.