Conceptual Flexible Aircraft Model for Modeling, Analysis and Control Studies-Reference-Cited by-同舟云学术

Conceptual Flexible Aircraft Model for Modeling, Analysis and Control Studies

Published:2010-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

da Silva Andre Luis¹,Paglione Pedro²,Yoneyama Takashi²

Affiliation:

1. Technological Institute of Aeronautics (ITA)

2. Technological Institute of Aeronautics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7806

Reference195 articles.

1. 2Dusto, A. R., Brune, G. W., Domfeld, G. M., Mercer, J. E., Pilet, S. C., Rubbert, P. E., Schwanz, R. C., Smutny, P., Tinoco, E. N., and Weber, J. A. “A method for predicting the stability characteristics of and elastic airplane,” Tech. Rep. CR-114712, NASA, 1974.

2. Hamilton's principle - Finite-element methods and flexible body dynamics

3. 4Karpel, M. “Design for Active and Passive Flutter Suppression and Gust Alleviation,” Tech. rep., NASA Contractor Report 3482, november 1981.

4. Flight dynamics of aeroelastic vehicles

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