Delay system identification applied to the longitudinal flight of an aircraft through a vertical gust

This paper deals with modelling and identification of aircraft dynamic entering a vertical gust. The identification approach initiated in (M. Fliess et al., 2003) falls under a prospect for identification from tests carried out in the Flight Analysis Laboratory of the DCSD of ONERA in Lille. The plane is considered into various elements which consist in the fuselage, the wing and the tail. The model incorporates delays linked to the aircraft passage through the atmospheric turbulence