Hello all,
I flew a plane with bad mag calibration in AUTO mode. At some moment the plane stall
this is not an issue by itself, but after the stall, the plane, instead of turning the throttle off, went full throttle and crashed into the ground really bad.
I want to implement some diagnosis to prevent that. For this I need to test this somehow.
Can I reproduce a stall on SITL?
As far as I know a pitch stall occurs when there is a divergence between the pitch demanded (increasing) and the pitch achieved (decreasing).
At the instant you indicate there is a discrepancy but the opposite; decreasing pitch demanded and increasing pitch achieved. And this is not a nose stall
A few moments later and at a much lower speed despite being nose down (engine cut?) a nose stall does occur.
Hello Lano,
thanks for the response.
I was investigating the TECS code and I can not understand what is going on with the engine here.
The plane by itself decreases throttle demand even though it started losing altitude
