uint8_t ao_flight_force_idle;
+/* Compute ADC value change given a defined pressure change in Pa */
+
+static inline int16_t
+ao_delta_pressure_to_adc(uint32_t pressure)
+{
+ static const double volts_base = AO_PRESSURE_VOLTS_BASE;
+ static const double volts_max = AO_PRESSURE_VOLTS_MAX;
+
+ /* Compute change in voltage from the sensor */
+ double volts = (double) pressure / AO_FULL_SCALE_PRESSURE * (volts_max - volts_base);
+
+ /* voltage divider in front of the ADC input to decivolts */
+ double adc_dv = volts * (10.0 * (double) AO_PRESSURE_DIV_MINUS /
+ ((double) AO_PRESSURE_DIV_PLUS + (double) AO_PRESSURE_DIV_MINUS));
+
+ /* convert to ADC output value */
+ double adc = adc_dv * AO_ADC_MAX / AO_ADC_REFERENCE_DV;
+
+ if (adc > AO_ADC_MAX)
+ adc = AO_ADC_MAX;
+ if (adc < 0)
+ adc = 0;
+
+ return (int16_t) adc;
+}
+
+#define AO_BOOST_DETECT ao_delta_pressure_to_adc(AO_BOOST_DETECT_PRESSURE)
+#define AO_QUIET_DETECT ao_delta_pressure_to_adc(AO_QUIET_DETECT_PRESSURE)
+
/*
* Landing is detected by getting constant readings from pressure sensor
* for a fairly long time (AO_INTERVAL_TICKS), along with the max being