* apogee detect
*/
ao_min_vel = abs(ao_flight_vel);
- ao_flight_state = ao_flight_apogee;
+ ao_flight_state = ao_flight_coast;
ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
}
break;
- case ao_flight_apogee:
+ case ao_flight_coast:
- /* apogee detect to drogue deploy:
+ /* apogee detect: coast to drogue deploy:
*
* accelerometer: abs(velocity) > min_velocity + 2m/s
* OR