Cruising Autopilot for a Flexible Aircraft with an Internal Loop of Model Following-Reference-Cited by-同舟云学术

Cruising Autopilot for a Flexible Aircraft with an Internal Loop of Model Following

Published:2014-03 Issue:2 Volume:27 Page:202-214
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Luís da Silva André¹,Paglione Pedro²,Yoneyama Takashi³

Affiliation:

1. Professor Adjunto I, Centro de Engenharia, Modelagem e Ciências Sociais Aplicadas, Univ. Federal do ABC, Santo André 09210-580, SP, Brazil (corresponding author).

2. Professor Associado, Aeronautics Engineering Division, Aeronautical Institute of Technology, São José dos Campos 12.228-900, SP, Brazil.

3. Full Professor, Electronics Engineering Division, Aeronautical Institute of Technology, São José dos Campos 12.228-900, SP, Brazil.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000277

Reference28 articles.

1. Robust H Design for Lateral Flight Control of Highly Flexible Aircraft

2. Linear Optimal Control

3. Aouf N. Boulet B. and Botez R. (2002). “Model and controller reduction for flexible aircraft preserving robust performance.” IEEE Trans. Control Syst. Technol. 10(2) 229–237.

4. da Silva A. L. (2010). “Nonlinear optimal model following control of flexible aircraft.” Ph.D. thesis Aeronautical Institute of Technology São José dos Campos SP Brazil.

5. da Silva A. L. Paglione P. and Yoneyama T. (2010a). “Conceptual flexible aircraft model for modeling analysis and control studies.” Proc. 2010 AIAA Atmospheric Flight Mechanics Conf. and Exhibit American Institute of Aeronautics and Astronautics (AIAA) Reston VA.

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