Development of a Modular, Generic Helicopter Flight Dynamics Model for Real-Time Simulation

Author:

Van Hoydonck Wim1,Pavel Marilena1

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference32 articles.

1. 1Advani, S. K., van Zuylen, E., and Bettendorf, S. "SIMONA - A Reconfigurable and Versatile Research Facility," Tech. Rep. AIAA-1997-3809, 1997.

2. 2van Gool, P. C. A., Customizing the Aerospatiale SA-330 Puma Flight Control System, M.Sc. Thesis,Delft University of Technology, Sept. 1992.

3. 3Voorsluijs, G. M. "Linear and Parameter-dependent Robust Control Techniques applied to a Helicopter UAV," Tech. Rep. AIAA-2004-4909, 2004.

4. 5Pavel, M. D., On the Necessary Degrees of Freedom for Helicopter and Wind Turbine Low-Frequency Mode Modeling, Ph.D. Thesis,Delft University of Technology, Delft, 2001.

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1. Flight Dynamics Modeling for a Small-Scale Flybarless Helicopter UAV;AIAA Atmospheric Flight Mechanics Conference;2011-06-14

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