Objective: Obtain models for unsteady aerodynamics of fixed-wing MAVs (e.g. incorporating dynamic stall, vortex shedding). Technical approach: Systematic models using approximate balanced truncation (balanced POD); empirical, phenomenological models that capture correct bifurcation behavior.
Unsteady Aerodynamic Models for Flight Control of Agile Micro Air Vehicles
2008
5 pages
Report
No indication
English
Aerodynamics , Aircraft , Models , Flight maneuvers , Remotely piloted vehicles , Unsteady aerodynamics , Control , Angle of attack , Truncation , Miniaturization , Fixed wing aircraft , Vortex shedding , Gusts , Mav(Micro air vehicles) , Balanced pod , Lcs(Lagrangian coherent structures) , Phenomenological models , Pod(Proper orthogonal decomposition) , Flight control
UNSTEADY AERODYNAMIC MODELS FOR AGILE FLIGHT AT LOW REYNOLDS NUMBER
British Library Conference Proceedings | 2010
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