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Shock and Vibration
Volume 19 (2012), Issue 5, Pages 939-946
http://dx.doi.org/10.3233/SAV-2012-0701

Application of the State-Dependent Riccati Equation and Kalman Filter Techniques to the Design of a Satellite Control System

L.C.G. Souza and R.G. Gonzáles

National Institute for Space Research- INPE, Brazilian Aeronautical Company-Embraer, 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 [5 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
  • 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
  • Huajiang Ouyang, and Dan Stancioiu, “Optimal vibration control of beams subjected to a mass moving at constant speed,” JVC/Journal of Vibration and Control, vol. 22, no. 14, pp. 3202–3217, 2016. View at Publisher · View at Google Scholar
  • Luiz C.G. Souza, and P. Bigot, “An adaptive method with weight matrix as a function of the state to design the rotatory flexible system control law,” Mechanical Systems and Signal Processing, 2016. View at Publisher · View at Google Scholar