I get that, though it also seems like it's the case that the Garmin/Dynon YD functionality will also try to coordinate, and that the flight control forces are so small on these light airplanes that it's OK for the two to be comingled (of course, in software, it is of course two different computations adding to the yaw servo command). <--- This is basically what I've gleaned from reading about RV10 rudder trim/YD, though I've not seen it really confirmed from Garmin, at least other than people mentioning the airplane stays coordinated with YD turned on.
I know Garmin has a note that their YD isn't designed to trim, but I'm wondering if that's really a disclaimer for if the airplane requires "too much" control input to stay coordinated in steady state. They want people to be aware that the servo's authority to coordinate in steady state (ie, trim) is minimal/"non existent" even through it will actually try. And thus, if an airplane with sufficiently light control forces is already mostly trimmed, the YD servo is actually sufficient in lieu of a dedicated spring/tab based trim system.