PDE Boundary Control for Flexible Articulated Aircraft Wings-Reference-Cited by-同舟云学术

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PDE Boundary Control for Flexible Articulated Aircraft Wings

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Paranjape Aditya¹,Chung Soon-Jo¹,Krstic Miroslav²

Affiliation:

1. University of Illinois, Urbana-Champaign

2. University of California, San Diego

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6486

Reference19 articles.

1. Parameterizing Stability Derivatives and Flight Dynamics with Wing Deformation

2. 4Ifju, P.G., Jenkins, D. A., Ettinger, S., Yongsheng L., Shyy, W., and Waszak, M. R. “Flexible-wing-based micro air vehicles,” AIAA 2002 - 0705.

3. Recent progress in flapping wing aerodynamics and aeroelasticity

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1. Vibration control of nonlinear three-dimensional length-varying string with input quantization;Journal of Vibration and Control;2020-02-12

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