This research is concerned with developing theory, algorithms. and applications of model -based, closed loop flow control in order to enable robust and agile flight of micro air vehicles, the efforts are centered around the application to integrated closed-loop flow and fight control for stabilization and regulations of separated flows occurring on unmanned and micro air vehicles ( UAV/MAV).
Closed-Loop Control of Vortex Formation in Separated Flows with Application to Micro Air Vehicles
2010
61 pages
Report
No indication
English
Aerodynamics , Aircraft , Fluid Mechanics , Closed loop systems , Flight control systems , Computational fluid dynamics , Drag reduction , Drones , Flight envelope , Gusts , Maneuverability , Miniaturization , Unsteady flow , Vortex shedding , Uav( unmanned air vehicle) , Mav(Micro air vehicle) , Flow control , Lift enhancement , Separated flows
CLOSED-LOOP CONTROL OF VORTEX SHEDDING IN A SEPARATED DIFFUSER USING AN INVERSE METHOD
British Library Conference Proceedings | 2004
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AIAA | 2002
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