I don't see how this system matches the description of subparagraph (A). The missile is fed a static gps coordinate at launch via the umbilical, and has no mechanism in the missile or launcher to "seek or proceed toward energy radiated or reflected from an aircraft or toward an image locating an aircraft" or "otherwise direct or guide the rocket or missile to an aircraft", which is the requirement in subparagraph A.

INAL, so I would like to understand why you think this applies?