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Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7613

Document Type: Article
Title: Simulation of wake vortex effects for UAVs in close formation flight
Authors: Saban, Deborah
Whidborne, J. F.
Cooke, A. K.
Issue Date: 2009
Citation: D. Saban, J.F. Whidborne. Simulation of wake vortex effects for UAVs in close formation flight. Aeronautical Journal, 2009, Volume 113, Issue 1149, pp727-738
Abstract: This paper addresses the development of multiple UAV deployment simulation models that include representative aerodynamic cross-coupling effects. Applications may include simulations of autonomous aerial refuelling and formation flying scenarios. A novel wake vortex model was developed and successfully integrated within a Matlab/Simulink simulation environment. The wake vortex model is both sufficiently representative to support studies of aerodynamic interaction between multiple air vehicles, and straightforward enough to be used within real time or near real time air-to-air simulations. The integration process is described, and simulation results of a two vehicles formation flight are presented.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7613
Appears in Collections:Staff publications - School of Engineering

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