Attenuation of Aircraft Flexible Modes during Maneuvering Flight-Reference-Cited by-同舟云学术

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Attenuation of Aircraft Flexible Modes during Maneuvering Flight

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control (GNC) Conference
language:
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Author:

Almeida Fabio¹,Silva Bruno²

Affiliation:

1. Aeronautics and Space Institute (IAE)

2. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5168

Reference30 articles.

1. 1Gates, S. and Lyon, H. “A Continuation of Longitudinal Stability and Control Analysis; Part I, General Theory,” Tech. Rep. 2027, H.M.S.O., 1944.

2. 3Milne, R. “Dynamics of the Deformable Aircraft; Parts I and II,” Tech. Rep. 3345, H.M.S.O., 1964.

3. Flight dynamics of aeroelastic vehicles

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