06.1 - Flight Dynamics and Control (Control & Modelling)
ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION
L.F. Zhao, Beihang University, Research Institute for Frontier Science, China; W.S. Wang, Beihang University, School of Automation Science and Electrical , China; Y.X. Chen, Beihang University, School of Aeronautic Science and Engineering, China; Z.X. Jiao, Beihang University, Ningbo Institute of Technology, China
This study concentrate on the control features and moddelling of the tail considering wing-tail interaction. New generation meshless numerical method is utilized and based on which the transient and cycle-averaged flow structure and aerodynamic force of the tail are analyzed. An analytical tail control force model is finally proposed and validated by simulation method.