Aircraft Control Based on Flexible Aircraft Dynamics-Reference-Cited by-同舟云学术

Aircraft Control Based on Flexible Aircraft Dynamics

Published:2017-01 Issue:1 Volume:54 Page:262-271
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Silvestre Flávio J.¹,Guimarães Neto Antônio B.¹,Bertolin Rafael Mendes¹,da Silva Roberto Gil Annes¹,Paglione Pedro¹

Affiliation:

1. Instituto Tecnológico de Aeronáutica, 12228-900 São José dos Campos-SP, Brazil

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033834

Reference10 articles.

1. BidinottoJ. H. “Proposta Conceitual de Excitador de Flutter Alternativo para Ensaios em Voo,” Ph.D. Dissertation, Univ. de São Paulo, São Paulo, Brazil, 2007.

2. SilvestreF. J., Methodology for Modelling the Dynamics of Flexible, High-Aspect-Ratio Aircraft in the Time Domain for Aeroservoelastic Investigations, 1st ed., Mensch and Buch Verlag, Berlin, 2013, pp. 9–72.

3. Guimarães NetoA. B. “Flight Dynamics of Flexible Aircraft Using General Body Axes: A Theoretical and Computational Study,” Ph.D. Dissertation, Inst. Tecnológico de Aeronáutica, São José dos Campos-SP, Brazil, 2014.

4. Aeroservoelastic Investigations of a High-Aspect-Ratio Motor Glider

5. Flight dynamics of aeroelastic vehicles

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