A flight computer that understands the flight
Most flight computers rely on barometric data for altitude estimation. These measurements can be disturbed during transonic flight or when pressure inside the avionics bay differs from the surrounding air. Vega combines accelerometer measurements with barometric data in a Kalman filter to estimate altitude and vertical velocity.
The filter runs at 100 Hz and adapts to the flight phase. During powered ascent, it relies primarily on the accelerometer, reducing the influence of pressure disturbances. During coasting, it gradually increases its reliance on the barometer as the rocket slows, correcting accumulated estimation drift and supporting apogee detection.
Vega also uses sustained acceleration to detect launch. Pressure changes during a long wait on the launchpad therefore do not trigger launch detection.
Together, these mechanisms help prevent misleading pressure readings from being mistaken for flight events and reduce their effect on altitude and velocity estimates.

