32th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

VIRTUAL FLIGHT TEST OF A BWB AIRCRAFT IN LOW SPEED WIND TUNNEL

B. Nieč, F. Cenč, Z. Liuč, T. Guoč, H. Sunč; čChina Aerodynamics Research and Development Center, China

This paper summarizes the virtual flight test of a BWB aircraft, which mainly aims to test and validate flight control laws using dynamical sub-scaled aircraft model, which is equipped with the flight control system. The effectiveness and performance of the Control Augmentation System is demonstrated via simulations and virtual flight test with the scenario of performing conventional maneuvers.


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