__pdata int16_t ao_raw_accel, ao_raw_accel_prev, ao_raw_pres;
__pdata int16_t ao_accel_2g;
+__xdata uint8_t ao_flight_force_idle;
+
/* Accelerometer calibration
*
* We're sampling the accelerometer through a resistor divider which
#define ACCEL_VEL_MACH VEL_MPS_TO_COUNT(200)
#define ACCEL_VEL_BOOST VEL_MPS_TO_COUNT(5)
-int32_t accel_vel_mach;
-int32_t accel_vel_boost;
-
/*
* Barometer calibration
*
ao_config_get();
ao_main_pres = ao_altitude_to_pres(ao_pres_to_altitude(ao_ground_pres) + ao_config.main_deploy);
ao_accel_2g = ao_config.accel_minus_g - ao_config.accel_plus_g;
- accel_vel_mach = ACCEL_VEL_MACH;
- accel_vel_boost = ACCEL_VEL_BOOST;
ao_flight_vel = 0;
ao_min_vel = 0;
ao_old_vel = ao_flight_vel;
/* Go to pad state if the nose is pointing up */
ao_config_get();
- if (ao_config.accel_plus_g != 0 && ao_config.accel_minus_g != 0 &&
- ao_flight_accel < ao_config.accel_plus_g + ACCEL_NOSE_UP)
+ if (ao_config.accel_plus_g != 0 &&
+ ao_config.accel_minus_g != 0 &&
+ ao_flight_accel < ao_config.accel_plus_g + ACCEL_NOSE_UP &&
+ !ao_flight_force_idle)
{
/* Disable the USB controller in flight mode
* to save power
/* disable RDF beacon */
ao_rdf_set(0);
+ /* Record current GPS position by waking up GPS log tasks */
+ ao_wakeup(&ao_gps_data);
+ ao_wakeup(&ao_gps_tracking_data);
+
ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
break;
}
ao_flight_init(void)
{
ao_flight_state = ao_flight_startup;
- ao_interval_min_accel = 0;
- ao_interval_max_accel = 0x7fff;
- ao_interval_min_pres = 0;
- ao_interval_max_pres = 0x7fff;
- ao_interval_end = AO_INTERVAL_TICKS;
-
ao_add_task(&flight_task, ao_flight, "flight");
}