Moment of Inertia for Crazyflie 2.0
Posted: Thu May 28, 2015 10:16 pm
Hello Bitcraze Community,
I am trying to create a closed-loop feedback control system for the Crazyflie 2.0, and I want to use Matlab to simulate the system dynamics. In order to do this, I need the quadcopter's moment of inertia I(xx),I(yy), and I(zz). Has anyone performed these calculations of the quad? If not, do you know of anyone else that has found said information?
-Tevon
I am trying to create a closed-loop feedback control system for the Crazyflie 2.0, and I want to use Matlab to simulate the system dynamics. In order to do this, I need the quadcopter's moment of inertia I(xx),I(yy), and I(zz). Has anyone performed these calculations of the quad? If not, do you know of anyone else that has found said information?
-Tevon