I doubt that.
There was a post -- that I assume was deleted -- that pointed out that when the taxiing F-313 made a turn, the rudders do not have matching deflections. Rudder pedals are coupled to the rudders even if the jet is fly-by-wire. On the ground where altitude and airspeed are near nil, rudder deflections are always at maximum whenever the rudders are activated during ground movements.
Likewise with the F-313's wings and canards. The flight controls system is a closed loop operation. On ground taxi, there should be stabilator and aileron deflections as the jet move over the paved but still uneven taxi ways. This is the effects of the gyroscope and accelerometers feedback loop. They have to be that sensitive. Further, on taxi, the system via the weight-on-wheel (WOW) switches, would automatically set the jet to take-off/land configuration. That means the flaps should deflected down to produce as much lift as possible.
This is from 5 yrs on the F-111 and 5 yrs on the F-16. I know how each jet feels and flies and even though there are decades of technology differences between the two jets, there are system commonalities that must exists.
When people suspect the F-313 is a 'fake', not all of them are out to troll Iran. Some like me observe with experienced eye and we find the F-313, to be kind about it, suspect.
Finally, just in case you think I make up the WOW switches...
http://www.askacfi.com/20020/squat-switch.htm
http://www.sciencedirect.com/science/article/pii/S1350630704001323