So you are referring to the pitot static boom, the pitot tube is now placed on the side of the radome, this is a function of the new AESEA radar being installed, space consideration has called for a not so unusual placement on the side. During prototype/testing phase they placed a static one on the nose tip, isolating the air speed reading from the AOA pitot, keeping the wiring simplified and making room for other data gatherers lets say (without getting into too many details
), its now back where it belongs as one complete unit. Therefore, yes a sign of great progress on radar and ancillary electronics but not really evidence or testament of "the stability of the aerodynamic characteristics, and the new FBW control system" as you said. The pitot tube will function just as well on the wing, nose or side of the aircraft as long as it is pointed forward.