case AltosLib.AO_LOG_FLIGHT:
state.set_flight(flight());
state.set_ground_pressure(adc_to_pa(idle_pres()));
+ state.set_accel_g(0, -1);
break;
case AltosLib.AO_LOG_STATE:
state.set_state(state());
break;
case AltosLib.AO_LOG_SENSOR:
state.set_pressure(adc_to_pa(pres()));
+ state.set_accel(firetwo_adc(thrust()) * 100);
break;
}
}