I was wondering why this system uses 2 differential sensors. I read the DOT/FAA/TC-18/7 study and they seem to indicate that one sensor was all that was needed.
top of page
FlyONSPEED.org Reduce Loss of Control Risk
Winner 2018 EAA Founder's Innovation Award and 2021 Grand Champion Winner
bottom of page
I need to read the study, but why not just one differential sensor for Pitot - AOA and one for q (Pitot - Static)? In the picture of the hardware board the Pitot and the AOA sensors are both referenced to static, and then a third (gauge) to measure static.
Finn