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Mathematical Problems in Engineering
Volume 2013, Article ID 257193, 8 pages
http://dx.doi.org/10.1155/2013/257193
Research Article

Design of the Microsatellite Attitude Control System Using the Mixed Method via LMI Optimization

Instituto Nacional de Pesquisas Espaciais (INPE), Avenida dos Astronautas 1758, 12227-101 So Jos Dos Campos, SP, Brazil

Received 5 April 2013; Revised 4 July 2013; Accepted 11 July 2013

Academic Editor: Maria Zanardi

Copyright © 2013 Erberson Rodrigues Pinheiro and Luiz Carlos Gadelha de Souza. 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.

Linked References

  1. X. C. Méndez Cubillos and L. C. G. de Souza, “Using of H-infinity control method in attitude control system of rigid-flexible satellite,” Mathematical Problems in Engineering, vol. 2009, Article ID 173145, 9 pages, 2009. View at Publisher · View at Google Scholar · View at Zentralblatt MATH · View at Scopus
  2. I. Mainenti, L. C. G. Souza, and F. L. Souza, “Design of a nonlinear controller for a rigid-flexible satellite using multi-objective generalized extremal optimization with real codification,” Shock and Vibration, vol. 19, pp. 1–10, 2012. View at Google Scholar
  3. L. C. G. Souza and R. G. Gonzalez, “Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system,” Shock and Vibration, vol. 19, pp. 22–28, 2012. View at Google Scholar
  4. D. S. Bernstein and W. M. Haddad, “LQG control with an H performance bound: a Riccati equation approach,” IEEE Transactions on Automatic Control, vol. 34, no. 3, pp. 293–305, 1989. View at Publisher · View at Google Scholar · View at Scopus
  5. P. P. Khargonekar and M. A. Rotea, “Mixed H2/H control: a convex optimization approach,” IEEE Transactions on Automatic Control, vol. 36, no. 7, pp. 824–837, 1991. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  6. T. P. Sales, D. A. Rade, and L. C. G. Souza, “Passive vibration control of flexible spacecraft using shunted piezoelectric transducers,” Aerospace Science and Technology, vol. 1, pp. 12–26, 2013. View at Publisher · View at Google Scholar
  7. C.-D. Yang and Y.-P. Sun, “Mixed H2/H state-feedback design for microsatellite attitude control,” Control Engineering Practice, vol. 10, no. 9, pp. 951–970, 2002. View at Publisher · View at Google Scholar · View at Scopus
  8. J. R. Wertz and W. J. Larson, Space Mission Analysis and Design, Microcosm Press, Hawthorne, Calif, USA, 1989.
  9. S. Boyd, L. El Ghaoui, E. Feron, and V. Balakrishnan, Linear Matrix Inequalities in System and Control Theory, SIAM Studies in Applied Mathematics, SIAM, Philadelphia, Pa, USA, 1994. View at MathSciNet