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Estimated altitude comes from three sources - barometer, GPS, and accelerometer. You can look at the black box logs to compare the three sensors and see which one might be off, if any. Particularly you might want to look at the accelerometer Z reading. Baro will drift slowly over time, and can be affected by airflow. But it tends to be good at distinguishing altitude changes over the course of a few seconds. It can have problems if the prop or ram air is pushing air into the fuselage, increasing the pressure in the fuselage. The GPS does not drift over time, but isn't precise or quick to react to sudden changes. GPS vertical accuracy is best when at least three constellations are enabled. The accelerometer quickly detects whether the aircraft is falling or rising, but is subject to noise from vibration. Vibration can therefore cause a sudden jump in the reported altitude. That jump will be corrected after a few seconds as the baro and GPS readings overcome the "ascent" reported by the accelerometer. |
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Excellent. If you've narrowed it down to barometer data, we'd want to look at air flow and pressure in the vicinity of the baro. The baro is of course measuring air pressure. Can we see a couple pics of the plane and any air openings into the fuselage? Also, this board isn't conformal coated, is it? |
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Ah yes, the baro will be affected by temperature. I'm not sure what would cause a spike like that, though. |
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I am going to start logging to black box and next time when I experience it, I will analyze that log. |
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During some longer flights (typically more than 40 minutes) with my plane equiped with FC SpeedyBee F405 wing mini (iNav 7.0.1) at the end of the flights in descend phase altitude readings (both OSD and logged in transmitter) fluctuate up and down randomly-see attached graph. I am afraid it is related with HW as I have not met this issue with Matek F411 wing mini FC in another plane. Have you ever experienced anything like this?

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