I am currently running an aircraft's mission with tilt-rotor as the mission inputs in vertical-take off & climb condition: So basically, in the configs setup I am giving the propeller thrust angle as 90 degrees and 45 degrees for the vertical take-off and climb conditions.
But upon running, I am getting an ValueError in this line: ut = ( Vz*np.cos(psi_2d) ) * rotation. Vz and cos(psi_2d) are of shape (15,24,20) but rotation is (3,).
So should I change the prop.rotation input with a (24,) shape np.array? Or maybe I am missing something here?