Can someone well versed in aerodynamics explain to me the canards that are a good part in the same level as the wings, or not very much higher than the wings. Life wise, canards should deflect air over the wing and keep the boundary layer from separating too early, to increase lift. Is that correct? In order for that to work, canards should, logically, be at least somewhat higher than the wing. Yet we have su-33, which needed extra lift to get off the carrier, and which has canards in the same level as wings. J20 here has somewhat higher positioned canards, mainly because of their anhedral angle compared to downhedral angle of the wings, but it is still a far cry from majority of canard/wing combos we see - like j10, rafale, typhoon, gripen, mig1.42, viggen, some mirage variants and so on.
I would assume it is also a matter of level of lift aid, lift efficiency and so on. And i'm sure there were other requirements, like RCS, in play. But, how much lift do canards add lift in su33 case and how much do they add in j20 configuration, compared to 'classical' high canard low wing combo?