27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-5.10.4

DYNAMIC MODELING AND CONTROL SYSTEM FOR A SHROUDED PROPELLER SYSTEM

Y. D. Jung, G. H. Kim, D. H. Shim, S. O. Park
KAIST, Korea

Keywords: shrouded propeller system, uav, dynamic modeling, classical control

For a vertical take-off and landing (VTOL) UAV such as a tail sitter, control system is a critical issue to stabilize the attitude of aircraft in crosswind. Therefore the main purpose in this paper is to focus on the control system design based on the aerodynamic analysis.

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