I have a rocket flight simulator that takes in aerodynamic coefficients defined relative to the vehicle body frame axes (Cx, Cy, Cz). These are in a lookup table based on mach.
I have some aerodynamic coefficients that are given relative to the wind frame (Cd, Cl), also with a lookup based on mach, and I would like to input these into the simulator.
Is there a good way to convert the coefficients to the body frame so that they can be compatible with my simulator?
I know that I could modify the simulator code to make the transformation at runtime, but I was wondering if there is a way to do it where I could convert the coefficient lookup table itself.