05.2 - Flight Dynamics and Control (UAV related)EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANEK. Fujitaš, H. Nagai, Tohoku University, Japan; A. Oyamaš; šISAS/JAXA, Japan This paper investigates the robustness of the aerial deployment behavior of the foldable-wing airplane for Mars exploration especially focused on the effect of the hinge axis tilting in a yaw direction. The tilted hinge axis design can deploy with low torque. The sideslip angle increase due to the hinge-axis tilting suppressed an aerodynamic force on the deploying wing. |