Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft - Part I: System Modeling-Reference-Cited by-同舟云学术

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Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft - Part I: System Modeling

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Meirovitch Leonard¹,Tuzcu Ilhan¹

Affiliation:

1. Virginia Tech

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4747

Reference24 articles.

1. The Expanding Domain of Aeroelasticity

2. J. B. Rea Co. "Aeroelasticity in Stability and Control," Wright Air DevelopmentCenter, TechnicalReport55-173,1957.

3. The Present Status of Aircraft Stability Problems in the Aeroelastic Domain

4. Ch. 9;Bisphinghoff R. L.,1962

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear aeroelastic analysis of a HALE aircraft with flexible components;Aerospace Science and Technology;2022-08

2. Integrated Flight Dynamic Modeling of Flexible Aircraft with Inertial Force-Propulsion-Aeroelastic Coupling;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

3. Dynamics and Adaptive Control for Stability Recovery of Damaged Asymmetric Aircraft;AIAA Guidance, Navigation, and Control Conference and Exhibit;2006-06-15

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