Designed and implemented a real-time active fin control system using PID control and IMU sensor fusion for rocket stabilization and guidance. Developed mathematical models and optimized control strategies to ensure stability during flight.
Built and tested a complete rocket system including custom PCB, servo-actuated fins, and multiple propulsion configurations. Successfully validated performance through wind tunnel testing and real flight experiments.
Designed, developed, and launched solid-propellant rockets reaching apogees of 2.6 km and 1.8 km. Conducted static thrust testing, aerodynamic optimization, and full system validation.
Designed a 19-seater amphibian aircraft based on the DHC-6 Twin Otter using XFLR5, OpenVSP, MATLAB and X-Plane for aerodynamic analysis and simulation.
Propulsion Laboratory
openFOAM