Right back at you: Do you have any evidence that DF-21D has been tested against a target like it was designed for? And please check up on the operational profile of the Pershing before you make another foolish and uninformed stated like "...Pershing couldn't even match the DF-21D in speed and guidance system during rentry of the atmosphere flight...."
".....The G&CC contained an inertial guidance system that could guide the missile on-target in a purely ballistic mode as a back-up.
The primary guidance system was a Goodyear Aerospace active radar guidance system. Using radar maps of the target area, the Pershing II had a reported accuracy of about 30 metres (100 ft) circular error probable.[according to whom?]
The reentry vehicle (RV) was structurally and functionally divided into three sections: the radar section (RS), the warhead section (WHS), and the guidance and control adapter (G&C) section. Quick access connectors made the all three of the RV sections replaceable at the launching site.
The radar section consisted of the radar unit with the antenna enclosed in an ablative radome.
The function of the radar unit was to transmit radio waves to the target area, to receive altitude and video information in return, and to send the detected video and altitude data to the digital correlator unit (DCU) located in the G&C section.
From:
That terminal radar system sounds exactly what the DF-21D is trying to do with its guidance trying to hit a carrier doesn't it? Now do you understand why I say that the father of the DF-21D is the Pershing 2?