Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability

Research paper by S. G. Parafes’

Indexed on: 30 Dec '15Published on: 30 Dec '15Published in: Russian Aeronautics (Iz VUZ)


An approach is proposed to solving the problem of collaborative design of the structure and stabilization system of a maneuverable unmanned aerial vehicle (UAV) taking into account the requirements of aeroelastic stability. The models and methods, which employ this approach, are described.