Identifiability of a nonlinear delayed-differential aerospace model

This technical note shows the identifiability of a nonlinear delayed-differential model describing aircraft dynamics. This result is obtained by an original combination: An extension of the results of Grewal and Glover to delay systems and an application of linear delayed-differential model identifiability of Orlov et al. . It requires initial conditions corresponding to an equilibrium state, which is implemented during the experimentation.