Development and Testing of Control Laws for the Active Aeroelastic Wing Program-Reference-Cited by-同舟云学术

Development and Testing of Control Laws for the Active Aeroelastic Wing Program

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Author:

Dibley Ryan¹,Allen Michael¹,Clarke Robert¹,Gera Joe²,Hodgkinson John³

Affiliation:

1. NASA Dryden Flight Research Center

2. Analytical Services & Materials, Inc.

3. Spiral Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6314

Reference10 articles.

1. 1Voracek, David, Pendleton, Ed, Reichenbach, Eric, Griffin, Dr. Kenneth, and Welch, Leslie, "The Active Aeroelastic Wing Phase I Flight Research Through January 2003,"NASA/TM-2003-210741,2003.

2. 2Lokos, William A., Olney, Candida D., Crawford, Natalie D., Stauf, Rick, and Reichenbach, Eric Y. "Wing Torsional Stiffness Testsof theActiveAeroelastic Wing F/A-18 Airplane,"NASA/TM-2002-210723,2002.

3. 3Lizotte, Andrew M. and Allen, Michael J. "Twist Model Development and Results From the Active Aeroelastic Wing F/A-18 Aircraft," NASA/TM-2005-212861,2005.

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