Detailed CAD Design: Detailed CAD modeling is performed for all components of the UAV, including the wings, fuselage, propeller, and control surfaces.
Material Selection and Structural Analysis: The materials to be used for the UAV’s structure are selected, and structural analyses are conducted.
Manufacturing Design: Design details for the UAV’s production, such as manufacturing plans, assembly instructions, and tolerances, are determined.
Electronics and Software Design: Work is carried out on the UAV’s electronic components and control software. Electronic materials are selected.
Detailed Aerodynamic Analysis: A detailed aerodynamic analysis of the UAV is performed. Performance results are evaluated and compared with the requirements. Performance parameters such as cruise speed, stall speed, maximum speed, required thrust power, flight time, moment coefficient, lift coefficient, drag coefficient, and stability are determined.