"The Design of a Real-Time Airspeed Transducer with CAN bus interfacing" was an Industry affiliates project conducted in partnership with RF Design. A pitot-static Airspeed sensor for UAV applications. Featuring CAN interfacing, 4 LPS22HB MEMS pressure sensors, STM32 MCU, and an EFM32WG MCU. The device calculates Angle of attack, CAS, Altitude, air density, temperature and static pressure. This information is then parsed through to a UART serial Port and CAN node.

I was responsible for the project management, hardware design and protobuild and programming over this 12-Week Program.