06.1 - Flight Dynamics and Control (Control & Modelling)
APPLICATION OF A MORE INTEGRATED TOTAL ENERGY CONTROL SYSTEM FOR IMPROVING AIRCRAFT AND ENGINE CONTROL EFFICIENCY
T. Giusti Degaspare, Embraer S.A., Brazil; K.H. Kienitz, Instituto Tecnológico de Aeronáutica, Brazil
This article presents improvements obtained by the integration of flight and engine controllers in terms of control efficiency with the use of the More Integrated Total Energy Control System (MI-TECS) and highlights how an integrated design framework offers advantages for controller design when compared with conventional control approaches.