printf ("\t\t\t\t\t%s accel %g vel %g alt %d main %d\n",
ao_state_names[ao_flight_state],
(ao_ground_accel - ao_flight_accel) / COUNTS_PER_G * GRAVITY,
(double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
ao_pres_to_altitude(ao_flight_pres) - ao_pres_to_altitude(ao_ground_pres),
ao_pres_to_altitude(ao_main_pres) - ao_pres_to_altitude(ao_ground_pres));
printf ("\t\t\t\t\t%s accel %g vel %g alt %d main %d\n",
ao_state_names[ao_flight_state],
(ao_ground_accel - ao_flight_accel) / COUNTS_PER_G * GRAVITY,
(double) ao_flight_vel / 100 / COUNTS_PER_G * GRAVITY,
ao_pres_to_altitude(ao_flight_pres) - ao_pres_to_altitude(ao_ground_pres),
ao_pres_to_altitude(ao_main_pres) - ao_pres_to_altitude(ao_ground_pres));