06.1 - Flight Dynamics and Control (Control & Modelling)
AILERON-FLAP-INTEGRATED ROLL CONTROL LAW BY OPTIMIZED CONTROL ALLOCATION FOR FLEXIBLE TRANSPORT AIRCRAFT
H. Wilke¹, G.C. Silva¹, F.J. Silvestre¹; ¹Technische Universität Berlin, Germany
In this paper a lateral path control law for a more flexible, single-aisle transport aircraft is designed. It is done by integrating and optimizing a control allocation algorithm using ailerons and flaps for roll control such that the influence of the flexibility on the rigid-body control is minimized.