Hey there guys, can anyone tell me how to calculate AoA and AoS for a flight computer that isn't primary? need that for a (maybe) future release. Help is much appreciated.
Hey there guys, can anyone tell me how to calculate AoA and AoS for a flight computer that isn't primary? need that for a (maybe) future release. Help is much appreciated.
@Grob0s0VBRa Thanks!
Edit: Is AoA not
V_Vert / V_Long?1)Take variables from this assembly.
2)Name the components in variable output of flight computer.
3)Copy these names to the variable setter
4) Now you can
V_Lat/V_Long- to find AOS andV_Lat/V_Vert- to find AOA.Maths. Can't explain it that easily.
You have to use it's position and rate of change of it's position to calculate a vector and stuff. I don't know.