ao_state_names[ao_flight_state],
(ao_flight_accel - ao_ground_accel) / COUNTS_PER_G * GRAVITY,
(double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
ao_state_names[ao_flight_state],
(ao_flight_accel - ao_ground_accel) / COUNTS_PER_G * GRAVITY,
(double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,