- state.flight_accel = (state.flight_accel * 15 + state.accel) / 16;
- state.flight_vel += (state.accel_plus_g - state.accel);
+ }
+ state.flight_accel = (state.flight_accel * 15 + state.accel) / 16;
+ if ((eeprom.seen & seen_sensor) == 0)
+ eeprom.sensor_tick = record.tick - 1;
+ state.flight_vel += (state.accel_plus_g - state.accel) * (record.tick - eeprom.sensor_tick);
+ eeprom.seen |= seen_sensor;
+ eeprom.sensor_tick = record.tick;
+ has_accel = true;
+ break;
+ case Altos.AO_LOG_PRESSURE:
+ state.pres = record.b;
+ state.flight_pres = state.pres;
+ if (eeprom.n_pad_samples == 0) {
+ eeprom.n_pad_samples++;
+ state.ground_pres = state.pres;