06.1 - Flight Dynamics and Control (Control & Modelling)
ADAPTIVE OUTPUT-FEEDBACK GAIN SCHEDULING APPLIED TO FLEXIBLE AIRCRAFT
R.M. Bertolin¹, A.B. Guimarães Neto¹, G.C. Barbosa¹, F.J. Silvestre¹; ¹Instituto Tecnológico de Aeronáutica, Brazil
The application of adaptive control will be demonstrated for a flexible aircraft in a dynamic gain scheduling approach. For that, an adaptive control law will be designed based on the Lyapunov stability theorems and making use of output feedback. Closed-loop nonlinear simulations and stability analyses will be performed.