06.1 - Flight Dynamics and Control (Control & Modelling)
IDENTIFICATION OF THE COMPLETE AERODYNAMIC MODEL OF A SUBSCALE FLIGHT TESTING
C. Fischer, ITA and IFSP, Brazil; L.M. Nepomuceno¹, E.A. Moura¹, R.G.A. da Silva¹, L.C.S. Góes¹; ¹ITA, Brazil
Subscale aircraft have been used for decades to design new aircraft, as well as to evaluate new design techniques. The acquisition of in-flight data from subscale aircraft is already possible today, such as a manned or fullscale aircraft. In this work is the implementation of a data acquisition system, data processing and system identification of the complete dynamic model of a Cessna 182 aircraft