/* Turn on telemetry system
*/
+ ao_rdf_set(1);
ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_PAD);
ao_flight_state = ao_flight_pad;
/* Increase telemetry rate */
ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_FLIGHT);
+ /* disable RDF beacon */
+ ao_rdf_set(0);
+
ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
break;
}
* 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
/* turn off the ADC capture */
ao_timer_set_adc_interval(0);
+ /* Enable RDF beacon */
+ ao_rdf_set(1);
ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
}
#define AO_VEL_COUNT_TO_MS(count) ((int16_t) ((count) / 2700))
static void
-ao_flight_status(void)
+ao_flight_status(void) __reentrant
{
printf("STATE: %7s accel: %d speed: %d altitude: %d main: %d\n",
ao_state_names[ao_flight_state],