Abstract 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.
Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability
Russian Aeronautics (Iz VUZ) ; 58 , 3 ; 271-278
2015-07-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability
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