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Dynamic Analysis of a Ducted Fan UAV in Forward Flight
Abstract:
This paper deals with the dynamic modeling of a ducted fan vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) and focuses on the dynamic characteristics analyzing in forward flight. A 6-DOF nonlinear model has been established in terms of the forces and moments and the model can be used in the structure and control system design.
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510-513
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Online since:
November 2012
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© 2012 Trans Tech Publications Ltd. All Rights Reserved
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