The J-20 two seater should have the most advanced layout. We should not expect J-20II to have the same. We know J-20II did have some interior changes, since that's what CAC said. However, they did start testing it in 2017. A lot of subsystems available when J-20 two seater was being developed were probably not available when J-20II design was frozen.
While I expect the J-20S to have the requisite modifications to support and enable the second seat in the cockpit, in terms of avionics systems (i.e.: including the actual physical hardware but also the software, everything from mission computers, to sensors, to datalinks), I would personally be surprised if there was any meaningful difference from J-20S to current in production J-20As.
J-20S would certainly have the tweaks to allow the second copilot/mission controller to use those same sensors and mission computers on its display consoles, but beyond that "duplication of key functions" I can't see why the systems would be different.
After all, looking from the outside the size of the various sensor apertures (and indeed the overall aircraft) looks identical between J-20A and J-20S save for one or two relocations likely related to the space rearrangement for the larger cockpit.
But any new advancement in avionics hardware or software should very easily be as useful for J-20A as for J-20S, and should fit in the same physical footprint as well.