06.1 - Flight Dynamics and Control (Control & Modelling)
SIMULATION ON THE EFFECT OF AIRCRAFT LOCAL STRUCTURE DAMAGES ON THE DYNAMIC DERIVATIVE COUPLING CHARACTERISTICS
B.-G. Mič, H. Zhanč, X. Baič, J.-Y. Yuč; čNorthwestern Polytechnical University, China
Two types of damaged models on the SACCON vehicle are constructed, and the SA-DES model is used to simulate the static and dynamic oscillations of the damaged models. The calculating method of the coupling dynamic derivatives due to the damaged configurations are developed and further analyzed.