VITO was a three-year long project handed down yearly from one team to another in the Faculty of Aerospace Engineering at the Technion, Israel, serving each as a group thesis project. I participated in the final year of VITO's development, which focused on full system simulation to be used in software and control design, leading to a series of flight experiments and culminating in free flight.

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The unmanned aircraft's configuration is a ducted fan, which consists of a single rotor within an airfoil-shaped duct (essentially, a rounded and closed wing), its control surfaces placed at the duct's trailing edge. This design allows for a relatively compact vehicle, capable of hovering and omnidirectional flight.

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During this project I was in charge of the 6DOF simulation of the system, which integrated experimental results and accounted for real-world hardware limitations and performance, and of control design. Additionally, I wrote flight software, including its deployment to the hardware, signal processing and implementation of safety features. I participated in all flight experiments, supporting them closely with analysis and live software adjustments.