Longitudinal Dynamics and Adaptive Control Application for an Aeroelastic Generic Transport Model-Reference-Cited by-同舟云学术

Longitudinal Dynamics and Adaptive Control Application for an Aeroelastic Generic Transport Model

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
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Author:

Nguyen Nhan¹,Tuzcu Ilhan²,Yucelen Tansel³,Calise Anthony³

Affiliation:

1. NASA Ames Research Center

2. California State University

3. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6291

Reference11 articles.

1. 2Calise, A. J., Yucelen, T., and Muse, J. A. “A Loop Recovery Method for Adaptive Control,” AIAA Guidance, Navigation, and ControlConference,AIAA2009-5967,August2009.

2. 3Hodges,D.H.andPierce,G.A.,IntroductiontoStructuralDynamicsandAeroelasticity,CambridgeUniversityPress,2002.

3. 4Nguyen, N. T. “Integrated Flight Dynamic Modeling of Flexible Aircraft with Inertial Force-Propulsion-Aeroelastic Coupling,” AIAA-2008-194,46thAIAAAerospaceSciencesMeeting,Reno,NV,Jan2008.

4. 5Houbolt, J. C. and Brooks, G. W. “Differential Equations of Motion for Combined Flapwise Bending, Chordwise Bending, and TorsionofTwistedNonuniformRotorBlades,”NACATechnicalNote3905,February1957.

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