Guidance, Navigation, And Control Engineer
CurrentDeveloped, implemented, and tested Spacecraft ADCS algorithms into FSW- From textbook to C++ GNC algs- Multiplicative Extended Kalman Filter estimating attitude and gyro bias, for both * 3-axis meas. (sun sensor + magnetometer) * Quaternion meas. (star-tracker)- EKF for magnetometer calibration- EKF for gyro calibration- GNC FSW state machine—autonomous.