since i'm totally new to the Autoquad platform as well asquadcopter systems, i would like to create a theoretical model of my Autoquad M4 v2 drone in order to understand the underlying physis.
Doing that, i need some parameters for modeling my Thrust and tourqe.
I know that thrust is related to tourque via a proportional relationship (k_m), and thrust is my angular velocity squard times another constant (k_t).
Can anyone of you guys provide me this constants or even the corresponding curves? I can't really perform any tests over her, because i don't got a test rig and so on.
In addition, can you tell me how this is linked to the drag coefficient?
My setup is: Autoquad M4 v2 ladybird with the standard corlessbrushed motors and the ladybird propellers.
Thanks a lot