Fixed Wing VTOL for Emergency Medical Vaccine Supply

Project Supervisor: Dr. Md. Ashraful Islam, Khulna University of Engineering & Technology, Bangladesh.

Timeline: September 2023 – March 2024

About Project: My supervisor secured a research grant from the University Grants Commission (UGC) of Bangladesh for this project, and I was selected as a research assistant due to my prior experience in the field.

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Fig. 1. Design of the UAV in SolidWorks

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Fig. 2. Flying Fixed-wing VTOL

The UAV was designed using SolidWorks 2023 and Blender3D, as shown in Fig. 1. The vehicle features a modular structure, allowing for easy disassembly and transportation. Its wings, fuselage, tail, and rudders can be individually detached. The frame was constructed using carbon fiber rods and plywood, with the plywood components cut into shape using a laser cutter. All mounting parts were 3D-printed using PLA, while the outer surface was made from Depron sheets.

The initial version of the UAV encountered several design issues, which were addressed before its test flight (Fig. 2). The vehicle successfully took off in both stabilize and GPS-guided modes, reaching an altitude of approximately 30 meters in VTOL mode. It then transitioned smoothly into fixed-wing flight and landed in VTOL mode (video). The total flight time was about 5 minutes, entirely in VTOL mode.


Design and source code from Jon Barron's website