Projects

Canard-based stabilization with STM32 flight computer, IMU/GPS, and gain-scheduled control.

Design and simulation of a closed-loop 3-axis AOCS using reaction wheels and thrusters for an autonomous spacecraft performing rendezvous and docking in GEO.

4-layer mixed-signal PCB: power distribution, sensors, connectors, ESD/TVS protection, routing constraints.

Three-satellite heliocentric constellation at Earth-Sun L4/L5 and Mars-Sun L5 for continuous solar weather monitoring and Earth–Mars communication relay. Orbit design and trajectory optimisation in Ansys STK.