Parametric Optimization of a Cyclogiro Aircraft Design for Efficient Hover with Aeroelastic Considerations
A minimization procedure is proposed to orient the design of a vertical take-off and landing drone towards sustainability.The vehicle is a novel cycloidal rotor drone and the principal objective is to yield the best ratio of payload to power consumption.The drone blades, rotor arms, and frame sara stedy stand aid are designed for fused deposition m