/* Main flight thread. */
enum ao_flight_state ao_flight_state; /* current flight state */
-uint16_t ao_boost_tick; /* time of most recent boost detect */
-uint16_t ao_launch_tick; /* time of first boost detect */
+AO_TICK_TYPE ao_boost_tick; /* time of most recent boost detect */
+AO_TICK_TYPE ao_launch_tick; /* time of first boost detect */
uint16_t ao_motor_number; /* number of motors burned so far */
#if HAS_SENSOR_ERRORS
* track min/max data over a long interval to detect
* resting
*/
-static uint16_t ao_interval_end;
+static AO_TICK_TYPE ao_interval_end;
#ifdef HAS_BARO
static ao_v_t ao_interval_min_height;
static ao_v_t ao_interval_max_height;
#define abs(a) ((a) < 0 ? -(a) : (a))
+#if !HAS_BARO
+// #define DEBUG_ACCEL_ONLY 1
+#endif
+
void
ao_flight(void)
{
#if HAS_ACCEL
if (ao_config.accel_plus_g == 0 ||
ao_config.accel_minus_g == 0 ||
- ao_ground_accel < ao_config.accel_plus_g - ACCEL_NOSE_UP ||
- ao_ground_accel > ao_config.accel_minus_g + ACCEL_NOSE_UP
+ ao_ground_accel < (accel_t) ao_config.accel_plus_g - ACCEL_NOSE_UP ||
+ ao_ground_accel > (accel_t) ao_config.accel_minus_g + ACCEL_NOSE_UP
#if HAS_BARO
|| ao_ground_height < -1000 ||
ao_ground_height > 7000
ao_wakeup(&ao_flight_state);
break;
+
+#if DEBUG_ACCEL_ONLY
+ case ao_flight_invalid:
+ case ao_flight_idle:
+ printf("+g %d ga %d sa %d accel %ld speed %ld\n",
+ ao_config.accel_plus_g, ao_ground_accel, ao_sample_accel, ao_accel, ao_speed);
+ break;
+#endif
+
case ao_flight_pad:
/* pad to boost:
*
*/
if (ao_height > AO_M_TO_HEIGHT(20)
#if HAS_ACCEL
- || (ao_accel > AO_MSS_TO_ACCEL(20) &&
- ao_speed > AO_MS_TO_SPEED(5))
+ || (ao_accel > AO_MSS_TO_ACCEL(20)
+ && ao_speed > AO_MS_TO_SPEED(5))
#endif
)
{
ao_flight_state = ao_flight_boost;
+ ao_wakeup(&ao_flight_state);
+
ao_launch_tick = ao_boost_tick = ao_sample_tick;
/* start logging data */
ao_gps_new = AO_GPS_NEW_DATA | AO_GPS_NEW_TRACKING;
ao_wakeup(&ao_gps_new);
#endif
-
- ao_wakeup(&ao_flight_state);
}
break;
case ao_flight_boost:
* (15 seconds) has past.
*/
if ((ao_accel < AO_MSS_TO_ACCEL(-2.5)) ||
- (int16_t) (ao_sample_tick - ao_boost_tick) > BOOST_TICKS_MAX)
+ (AO_TICK_SIGNED) (ao_sample_tick - ao_boost_tick) > (AO_TICK_SIGNED) BOOST_TICKS_MAX)
{
#if HAS_ACCEL
#if HAS_BARO
#else
ao_flight_state = ao_flight_coast;
#endif
- ++ao_motor_number;
ao_wakeup(&ao_flight_state);
+ ++ao_motor_number;
}
break;
#if HAS_ACCEL && HAS_BARO
* number of seconds.
*/
if (ao_config.apogee_lockout) {
- if ((int16_t) (ao_sample_tick - ao_launch_tick) <
- AO_SEC_TO_TICKS(ao_config.apogee_lockout))
+ if ((AO_TICK_SIGNED) (ao_sample_tick - ao_launch_tick) <
+ (AO_TICK_SIGNED) AO_SEC_TO_TICKS(ao_config.apogee_lockout))
break;
}
#endif
)
{
-#if HAS_IGNITE
- /* ignite the drogue charge */
- ao_ignite(ao_igniter_drogue);
-#endif
-
+ /* enter drogue state */
+ ao_flight_state = ao_flight_drogue;
+ ao_wakeup(&ao_flight_state);
#if HAS_TELEMETRY
/* slow down the telemetry system */
ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_RECOVER);
/* Turn the RDF beacon back on */
ao_rdf_set(1);
#endif
-
- /* and enter drogue state */
- ao_flight_state = ao_flight_drogue;
- ao_wakeup(&ao_flight_state);
}
else
#else /* not HAS_BARO */
#define MAX_QUIET_ACCEL 2
- if ((int16_t) (ao_sample_tick - ao_interval_end) >= 0) {
+ if ((AO_TICK_SIGNED) (ao_sample_tick - ao_interval_end) >= 0) {
if (ao_interval_max_accel_along - ao_interval_min_accel_along <= ao_data_accel_to_sample(MAX_QUIET_ACCEL) &&
ao_interval_max_accel_across - ao_interval_min_accel_across <= ao_data_accel_to_sample(MAX_QUIET_ACCEL) &&
ao_interval_max_accel_through - ao_interval_min_accel_through <= ao_data_accel_to_sample(MAX_QUIET_ACCEL))
{
ao_flight_state = ao_flight_landed;
+ ao_wakeup(&ao_flight_state);
#if HAS_ADC
/* turn off the ADC capture */
ao_timer_set_adc_interval(0);
#endif
-
- ao_wakeup(&ao_flight_state);
}
/* Reset interval values */
*/
if (ao_height <= ao_config.main_deploy)
{
-#if HAS_IGNITE
- ao_ignite(ao_igniter_main);
-#endif
+ ao_flight_state = ao_flight_main;
+ ao_wakeup(&ao_flight_state);
/*
* Start recording min/max height
ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS;
ao_interval_min_height = ao_interval_max_height = ao_avg_height;
-
- ao_flight_state = ao_flight_main;
- ao_wakeup(&ao_flight_state);
}
break;
if (ao_avg_height > ao_interval_max_height)
ao_interval_max_height = ao_avg_height;
- if ((int16_t) (ao_sample_tick - ao_interval_end) >= 0) {
+ if ((AO_TICK_SIGNED) (ao_sample_tick - ao_interval_end) >= 0) {
if (ao_interval_max_height - ao_interval_min_height <= AO_M_TO_HEIGHT(4))
{
ao_flight_state = ao_flight_landed;
-
+ ao_wakeup(&ao_flight_state);
#if HAS_ADC
/* turn off the ADC capture */
ao_timer_set_adc_interval(0);
#endif
-
- ao_wakeup(&ao_flight_state);
}
ao_interval_min_height = ao_interval_max_height = ao_avg_height;
ao_interval_end = ao_sample_tick + AO_INTERVAL_TICKS;
#if HAS_FLIGHT_DEBUG
case ao_flight_test:
#if HAS_GYRO
- printf ("angle %4d pitch %7d yaw %7d roll %7d\n",
+ printf ("angle %4d pitch %7ld yaw %7ld roll %7ld\n",
ao_sample_orient,
((ao_sample_pitch << 9) - ao_ground_pitch) >> 9,
((ao_sample_yaw << 9) - ao_ground_yaw) >> 9,
printf ("sample:\n");
printf (" tick %d\n", ao_sample_tick);
- printf (" raw pres %d\n", ao_sample_pres);
+#if HAS_BARO
+ printf (" raw pres %ld\n", ao_sample_pres);
+#endif
#if HAS_ACCEL
printf (" raw accel %d\n", ao_sample_accel);
#endif
- printf (" ground pres %d\n", ao_ground_pres);
- printf (" ground alt %d\n", ao_ground_height);
+#if HAS_BARO
+ printf (" ground pres %ld\n", ao_ground_pres);
+ printf (" ground alt %ld\n", ao_ground_height);
+#endif
#if HAS_ACCEL
printf (" raw accel %d\n", ao_sample_accel);
printf (" groundaccel %d\n", ao_ground_accel);
printf (" accel_2g %d\n", ao_accel_2g);
#endif
- printf (" alt %d\n", ao_sample_alt);
- printf (" height %d\n", ao_sample_height);
+#if HAS_BARO
+ printf (" alt %ld\n", ao_sample_alt);
+ printf (" height %ld\n", ao_sample_height);
+#endif
+
#if HAS_ACCEL
printf (" accel %d.%02d\n", int_part(accel), frac_part(accel));
#endif
printf ("kalman:\n");
- printf (" height %d\n", ao_height);
+ printf (" height %ld\n", ao_height);
printf (" speed %d.%02d\n", int_part(ao_speed), frac_part(ao_speed));
printf (" accel %d.%02d\n", int_part(ao_accel), frac_part(ao_accel));
- printf (" max_height %d\n", ao_max_height);
- printf (" avg_height %d\n", ao_avg_height);
- printf (" error_h %d\n", ao_error_h);
+ printf (" max_height %ld\n", ao_max_height);
+ printf (" avg_height %ld\n", ao_avg_height);
+ printf (" error_h %ld\n", ao_error_h);
#if !HAS_ACCEL
printf (" error_avg %d\n", ao_error_h_sq_avg);
#endif
ao_orient_test_select(void)
{
ao_orient_test = !ao_orient_test;
+ printf("orient test %d\n", ao_orient_test);
}
const struct ao_cmds ao_flight_cmds[] = {