Some people believe J7W to be maneuverable, even tho it's clearly an impossible case for the plane. The said vehicle has 240kg/m2 wing loading with only 20.5m2 wingsurface area available, canard itself isn't a bad thing tho. It's just too heavy for the overall profile, and the weight is coming from the decently complex air-cooling system. Empty weight of 3600kg with 5000kg TOW(the added weight is mostly the cooling water) is simply ridiculous for a combatant aircraft. I mean, J7W is a tandem plane(main lift set aft of the CoG) with very small fore-wings.
The canards are overly-loaded to accommodate with the possible wing-first stall, as long as the canards are stalling first it's easier to recover from the nose-up state. So the canards are restricted to the limitation dependents of the rear wing's capability. In this case, high wing-loading with low-aspect ratio wing combination is just... just bad. Can they even perform a stable barrel-roll? It's another question. Only if they can put a wider, yet bigger canards for the plane, it might be a different story but, this isn't a case.
Nevertheless, there is no any other look-alike so. The fans got the idea of [canard aircrafts being maneuverable]
...is just the jet-era stereotype. It's meant to be a high-altitude interceptor so I really don't see the points in the low-aspect ratio wings, shouldn't they use a wider wing profile much like Ta152 or other reconnaissance military aircrafts(with that wing configuration, the exceptional energy retention is way worse).
I mean. the reduced drag from the frontal-area won't make-up for it really. Only thing good about it is just the reduced stall-limit combined with better climb-rate for the same amount of thrust. Aghhh, J7W is over-rated, It's no match for 1600hp Xp-55(Planned).