Wing Support Structure LSU03 UAV Strengthen for Dynamic Load

LSU03 UAV was resulted by Aeronautics Technology Center, National Institute of Aeronautics and Space, LAPAN. This UAV has flight scenario like small UAV comprising taxi moves, take off, cruising, descending and landing. The operational of this craft was appeared stress structure specially wing support structure. The appearing of this stress was caused by the dynamic load or shock loads which the biggest at early landing and first touchdown in ground plane. With the dimensional data of wing support structure, analytical method, mission objective research and flight operational of LSU03 can be known that the structure can fulfill mission that is robust, light and strength. E-glass composite material was used as material of the wing support structure. This structure is strengthen receive dynamic load during flight time and landing.