06.1 - Flight Dynamics and Control (Control & Modelling)
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
J. Lee¹, S. Kim¹, S. Jung¹, H. Lee¹, Y. Kim¹; ¹Seoul National University, South Korea
An autopilot design is proposed for an asymmetric variable-span morphing aircraft. The integrated flight control system is designed based on dynamic inversion. Asymmetric morphing is used for roll control, while symmetric morphing is for flight performance optimization and direct force control. Numerical simulation results demonstrate the effectiveness of the proposed scheme.