I'm currently building a plane that needs more angle on the control surface at a speed threshold.
I've tried
Pitch*0.5 + Trim*0.07 + Roll*0.5 - (abs(TAS>390) ? PitchRate*0.005 : PitchRate*0.05)
which doesn't function.
and
Pitch*0.5 + Trim*0.07 - Roll*0.5 - IAS>375 ? PitchRate*0.005 : PitchRate*0.05
which only causes the control surface to spazz out.
If you're interested, here.
Thanks.
Judging from the spaghetti...
You should try multiplying instead of subtracting.
Pitch*.5*(f(IAS))+Trim*.07+Roll*.5Where f(IAS) is some function of your airspeed. This should be more gradual and less spazzy if f(IAS) doesn't involve the
Condition ? True : False. A clamped linear or exponential function should do.