Technical Design and Modeling with SolidWorks

Aerodynamic Optimization: Detailed form adjustments were made at the fuselage and wing junctions to minimize the aircraft's drag coefficient. Assembly and Interference Analysis: The placement of all electronic components and mechanical parts within the fuselage was simulated to resolve potential interferences. Center of Gravity Validation: Material densities for each designed component were integrated into the system to digitally verify the center of gravity, which is vital for flight stability.