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Multidisciplinary design optimization of an electric propulsion system of a hybrid UAV considering wind disturbance rejection capability in the quadrotor mode

EngineeringAerial RoboticsElectric Propulsion SystemMultidisciplinary Design OptimizationAerospace EngineeringUnmanned SystemSystems EngineeringAerodynamicsFlying RobotAerospace Propulsion SystemsPropulsionAir Vehicle SystemFlight ControlUnmanned Aerial VehiclesHybrid Uav