Matematizzando il tutto e scopiazzando da RCGroup quindi...
Citazione:
cc: cyclic constant
pc: pitch constant
a = cc * ( elevator * cos (alpha + 0) + aileron * cos (alpha + 90) ) + pc * pitch
b = cc * ( elevator * cos (alpha + 120) + aileron * cos (alpha + 210) ) + pc * pitch
c = cc * ( elevator * cos (alpha + 240) + aileron * cos (alpha + 330) ) + pc * pitch
|
