ao_microflight(void)
{
int16_t sample_count;
+ int16_t log_count;
uint16_t time;
uint32_t pa_interval_min, pa_interval_max;
int32_t pa_diff;
- uint8_t h, i;
+ uint8_t h;
+ uint8_t i;
uint8_t accel_lock = 0;
uint32_t pa_sum = 0;
}
/* Log the remaining samples so we get a complete history since leaving the ground */
- for (; i != h; i = SKIP_PA_HIST(i,2)) {
+#if LOG_INTERVAL < NUM_PA_HIST
+ for (; i != h; i = SKIP_PA_HIST(i,2))
+#endif
+ {
pa = pa_hist[i];
ao_log_micro_data();
}
/* Now sit around until the pressure is stable again and record the max */
sample_count = 0;
+ log_count = 0;
pa_min = ao_pa;
pa_interval_min = ao_pa;
pa_interval_max = ao_pa;
ao_microsample();
if ((sample_count & 3) == 0)
ao_led_off(AO_LED_REPORT);
- if (sample_count & 1)
+ if (log_count == LOG_INTERVAL - 1) {
ao_log_micro_data();
+ log_count = 0;
+ } else
+ log_count++;
/* If accelerating upwards, don't look for min pressure */
if (ao_pa_accel < ACCEL_LOCK_PA)