Design and construction of a novel quad tilt-wing UAV

Mechatronics

Volumn 22, Issue 6, 2012, Pages 723-745

  Cetinsoy, E ^a   Dikyar, S ^a   Hancer, C ^a   Oner, K T ^a   Sirimoglu, E ^a   Unel, M ^a   Aksit, M F ^a  

^a SABANCI UNIVERSITY   (Turkey)

Author keywords

Aerodynamic design; Carbon composite; Hierarchical control system; Quad tilt wing; UAV

Indexed keywords

AERODYNAMICS; AIRCRAFT CONTROL; AIRCRAFT LANDING; ALTITUDE CONTROL; ANTENNAS; CARBON CARBON COMPOSITES; CONTROLLERS; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; LEVEL CONTROL; UNMANNED AERIAL VEHICLES (UAV);

AERODYNAMIC DESIGNS; CARBON COMPOSITE MATERIALS; CARBON COMPOSITES; DESIGN AND CONSTRUCTION; HIERARCHICAL CONTROL SYSTEMS; NEWTON EULER FORMULATION; TILT-WINGS; VERTICAL TAKE-OFF AND LANDINGS;

WINGS;

EID: 84866108368     PISSN: 09574158     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.mechatronics.2012.03.003     Document Type: Conference Paper

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