An offline-calibrated propulsion database plus an online search algorithm automatically selects components and battery/airframe parameters for electric multicopters that meet target flight time, payload, altitude, and maneuverability.
An optimal approach to the preliminary design of small hybrid-electric aircraft,
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Design Automation and Optimization Methodology for Electric Multicopter UAVs
An offline-calibrated propulsion database plus an online search algorithm automatically selects components and battery/airframe parameters for electric multicopters that meet target flight time, payload, altitude, and maneuverability.