Is there something particularly strange about them being small?
Brief summary from parts of the article:
All-moving tail fins were used to increase control surface area under supersonic conditions.
The vortex created at the front of the aircraft body will create a tendency for the tail section to swerve (like when you pull up the nose slightly and then roll)
This causes the plane tail section and tail rudder to experience a downward pressure, affecting adversely its vertical stability under high angle of attack. Making the nose of the plane hard to press downward. (in extreme cases it will do a flip and enter tail spin)
To solve this problem, the size of the tail is reduced from 20-25% to 10-13% (it didn't say with respect to what)
The tail is swept back due to consideration of the area rule, as the J-20 cannot extend it's horizontal stabilizers past the abrupt change in cross sectional area after the engine nozzle (like F-22 can) (since it uses canards instead)
F-22 and T-50 use slightly forward "butterfly tail", this is to reduce the blockage of tail surface by the aircraft body at high AoA. J-20 does not need to consider this because it had canards
hope this helps.