This system is similar to the new GPS based attitude you can select on our EFIS systems either as sole attitude or as reference for a real AHRS.
Taking advantage of the Swiss made u-Blox GPS receiver the EFIS has access to internals way beyond what is available on NMEA strings, including a very accurate 3D velocity vector.
This means you can create a reasonable AHRS display (very reasonable actually) that is not unlike the aiding information used with some high-end aided gyro based systems (except you ditch the gyros and look directly at the aiding information).
This system too, describes your path though the air and is not capable of showing pitch up near the stall. Of course - that could be faked but we decided to not after our many test flights. The reason for this is that it started making sense rather quickly. It's a case of the pilot understanding what he is seeing and then using it correctly.
In order to avoid infringing patents our system adds other sensor inputs as well and takes advantage of the fast operation of a modern GPS receiver.
As a cross-check to an existing gyro based AHRS it is great (and you don't need an expensive EFIS for this, our little sub-$1000 XTreme can do this as well).
The main reason it is great as a cross check is that it is based on completely different technology and neither suffers from the potential problems of the other.
Rainier
CEO MGL Avionics
Quote:
Originally Posted by Alan Carroll
Yesterday I went out and tested how a static leak would affect the ADI, by opening the alternate static source I have installed (which vents to the cockpit). The sudden decrease in static pressure caused a pitch up, as Paul noted in the OP. However after about 10-12 seconds the pitch indication stabilized as the instrument adjusted to the new lower pressure. So, ultimately a static leak doesn't seem to pose a problem so long as it is a stable leak. What the ADI cares about it rate of change.
On the other hand I found I could rather easily "fake out" the ADI at speeds as high as 80 knots, by using a very low power setting. This results in nose-up attitude but a nose-down indication on the ADI (due to loss of altitude). The ADI continues to accurately indicate the actual flight path though. Like someone said earlier, you need to understand what this instrument is telling you.
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