Let's see if we can unravel this. First off, the rudder. The control cables will run from the rudder bar or pedals along the inside of the fuselage at the bottom, guided either by pulleys or fairleads to follow the fuselage structure. They will exit the fabric through a grommet pretty much in a straight line from the control horn on the rudder to the fuselage side.
Elevators can go a couple of ways. If the elevators have a control horn out along the surface somewhere, then the cable will run in a straight line from there to the fuselage skin, and enter through a grommet.
Ailerons are where it gets convoluted. On WWl airplanes, the control cables usually ran inside the wing, from the control horn on the aileron, into the wing, around a pulley, then to another pully in the wing center section, then down into the fuselage. They would be routed along the cabane struts on the outside with fairleads, or simply drop straight into the fuselage from the wing center section. But they all were different, all depends on the internal structure of the wing.
Hope this helps!