A Novel Force Control Traverse for Simulating UAV Flight in a Wind Tunnel-Reference-Cited by-同舟云学术

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A Novel Force Control Traverse for Simulating UAV Flight in a Wind Tunnel

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Muse Jonathan¹,Kutay Ali¹,Calise Anthony¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6714

Reference19 articles.

1. Grid Graphical Analysis Package (GridGAP) for store separation testing at AEDC

2. 5Wilhelm, K.andGmelin, B. “DynamicWindTunnelTestingforActiveControlResearch,”AGARDograph, Vol.AG-262, Dec. 1984.

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1. Minimally Constrained Flight Simulation in Wind Tunnel;Journal of Aircraft;2019-07

2. Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig;Journal of Aircraft;2019-05

3. Simulation of Rapidly Maneuvering Airfoils with Synthetic Jet Actuators;AIAA Journal;2013-08

4. A discrete-vortex model for the arbitrary motion of a thin airfoil with fluidic control;Journal of Fluids and Structures;2011-07

5. Vortex Model Based Adaptive Flight Control Using Synthetic Jets;AIAA Guidance, Navigation, and Control Conference;2009-06-14

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