/* Landing is detected by getting constant readings from both pressure and accelerometer
* for a fairly long time (AO_INTERVAL_TICKS)
*/
-#define AO_INTERVAL_TICKS AO_SEC_TO_TICKS(5)
+#define AO_INTERVAL_TICKS AO_SEC_TO_TICKS(10)
#define abs(a) ((a) < 0 ? -(a) : (a))
ao_interval_max_height = ao_avg_height;
if ((int16_t) (ao_sample_tick - ao_interval_end) >= 0) {
- if (ao_interval_max_height - ao_interval_min_height <= AO_M_TO_HEIGHT(2))
+ if (ao_interval_max_height - ao_interval_min_height <= AO_M_TO_HEIGHT(4))
{
ao_flight_state = ao_flight_landed;