Designed and implemented a real-time active fin control system using PID control and IMU sensor fusion for rocket stabilization and guidance.
Designed, developed, and launched solid-propellant rockets reaching apogees of 2.6 km and 1.8 km.
Designed a 19-seater amphibian aircraft based on the DHC-6 Twin Otter using XFLR5, OpenVSP, MATLAB and X-Plane.
Propulsion Laboratory
openFOAM