Cpt’s Stability controller (Aircraft)
Simple and tunable stability controller
Roll divide:
Limits the max banking the plane can do
value 1: 45 degree max banking
value 1.9-2: 90 degree max banking
Pitch divide:
Same as roll divide but in the pitch axis (recommended to keep it at 2)
value 1: 90 degree max pitch (not recommended. Causes the controller to freak out)
value 2: 45 degree max pitch
