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Shock and Vibration
Volume 19, Issue 5, Pages 947-956

Design of a Nonlinear Controller for a Rigid-Flexible Satellite Using Multi-Objective Generalized Extremal Optimization with Real Codification

I. Mainenti-Lopes, L.C.G. Souza, and F.L. De Sousa

National Institute for Space Research, Space Mechanics and Control Division, São Jose dos Campos, SP, Brazil

Received 25 April 2012; Accepted 25 April 2012

Copyright © 2012 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [4 citations]

The following is the list of published articles that have cited the current article.

  • Erberson Rodrigues Pinheiro, and Luiz Carlos Gadelha de Souza, “Design of the Microsatellite Attitude Control System Using the Mixed Method via LMI Optimization,” Mathematical Problems in Engineering, vol. 2013, pp. 1–8, 2013. View at Publisher · View at Google Scholar
  • Alain G. de Souza, and Luiz C. G. de Souza, “Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics,” Mathematical Problems in Engineering, vol. 2014, pp. 1–8, 2014. View at Publisher · View at Google Scholar
  • Valentino Lau, Fabiano Luis de Sousa, Roberto Luiz Galski, Evandro Marconi Rocco, José Carlos Becceneri, Walter Abrahão dos Santos, and Sandra Aparecida Sandri, “A multidisciplinary design optimization tool for spacecraft equipment layout conception,” Journal of Aerospace Technology and Management, vol. 6, no. 4, pp. 431–446, 2014. View at Publisher · View at Google Scholar
  • A G de Souza, and L C G de Souza, “H infinity controller design to a rigid-flexible satellite with two vibration modes,” Journal of Physics: Conference Series, vol. 641, pp. 012030, 2015. View at Publisher · View at Google Scholar