An integrated engine control unit designed to fire and control liquid bi-propellant rocket engines.
Custom 4-layer interrupter control board for DRSSTC systems. STM32F405-based, fiber-optically isolated outputs, hardware E-brake safety chain, and controlled-impedance routing (90Ω USB, 50Ω FSMC/SDIO). Designed in KiCad 9.0.
Thrust vector control rocket via differentiable simulation and reinforcement learning.