Aerodynamics and Wakes: Moving Toward Higher Fidelity in Flight Simulation 

Dr. Keller is an Associate with Continuum Dynamics, Inc. (CDI), an R&D boutique providing high quality, cost effective engineering services and state-of-the-art technical solutions for government and industry. Dr. Keller has been active in the research and development of aircraft and helicopter flight dynamics since the 1990s, including leading research into low-order inflow models for helicopters that capture fundamental cross-coupling behavior, in particular the coupled roll-pitch response characteristics in low speed flight. While at CDI, Dr. Keller has led and supported several flight dynamics and simulation software development projects, including projects in aircraft flight controls, V-22 icing detection and simulation demonstration, and ship airwake modeling for helicopter-ship dynamic interface (DI) simulation. His most recent work has been in unmanned air vehicle (UAV) flight dynamics modeling, detection, and recovery from aerodynamic disturbances (upsets), as well as in real-time aeroelastic and aeroservoelastic models for fixed wing aircraft. 

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