05.2 - Flight Dynamics and Control (UAV related)
ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR RECONFIGURATION OF ORGANIC FLIGHT ARRAY
J. Jeong¹, S. Kim¹, J. Suk¹; ¹Chungnam National University, South Korea
This paper presents a control system for the organic flight array(OFA). The OFA is able to be assembled or separated by ducted-fan modules. Physical parameters of the OFA change during the mission according to the reconfigurable feature. To cope with these uncertainties, a sliding mode control technique is used with applying an adaptive law. The performance is verified via numerical simulations.