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It's almost surely from DCS. This mod was developed very lazily with a low-fidelity model based on publically-available data, to produce lookup tables fed with guesstimated and whimsical figures that in no way reproduce the real prototypes' behavior.


However, I don't know why you are surprised by the 25° AoA at low altitude? The two PAVs should be able to pull that (and some) thanks to the YF-23's nose chines. I have produced CFD data of the forebody that support this.


The ginormous ruddervators should also be sufficiently-dimensioned to produce the required pitching moment.


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