A mismatch function is used to check the validity of a low-order equiv
alent system model that has been derived from a high-order system repr
esentation. If the difference between the low- and high-order models i
s greater than allowed by the mismatch function, the flying qualities
predictions obtained from parameters of the low equivalent system may
not be representative of the ratings a pilot would give the actual air
craft. A methodology is developed in this paper to derive equivalent s
ystem mismatch functions analytically. The methodology is used to anal
ytically determine a mismatch function for the longitudinal axis of a
class IV fighter aircraft in the category A, nonterminal flight phase.