28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
EVALUATION OF DYNAMIC BEHAVIOR OF A DEPLOYABLE WING UAV BY DROP TEST
Tohoku Univ., Japan
Keywords: deployable wing, uav, drop test, balloon, dynamic behavior
Aerial deployment technique is required for next-generation airplanes. Dynamic behavior of an airplane during a deployment motion is one of the big problems. In order to evaluate this, a drop test via a balloon was performed for a UAV which has a foldable wing. Flight data and animation were analyzed.
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