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Mathematical Problems in Engineering
Volume 2014, Article ID 471352, 12 pages
http://dx.doi.org/10.1155/2014/471352
Research Article

Designing a Robust Nonlinear Dynamic Inversion Controller for Spacecraft Formation Flying

1Center for ICT and Automobile Convergence, Kyungpook National University, Daegu 702-701, Republic of Korea
2School of Electronics Engineering, Kyungpook National University, Daegu 702-701, Republic of Korea

Received 18 April 2014; Accepted 1 July 2014; Published 17 July 2014

Academic Editor: Vivian Martins Gomes

Copyright © 2014 Inseok Yang et al. 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. Y. Lv, Q. Hu, G. Ma, and J. Zhou, “6 DOF synchronized control for spacecraft formation flying with input constraint and parameter uncertainties,” ISA Transactions, vol. 50, no. 4, pp. 573–580, 2011. View at Publisher · View at Google Scholar · View at Scopus
  2. D. Forta, F. Bordi, and C. Scolese, “Low-cost minimum size satellites for demonstration of formation flying modes at small, kilometer-size distance,” in Proceedings of the 13th AIAA/USU Conference on Small Satellite, SSC99-VI-3, pp. 1–15, 1999.
  3. M. S. De Queiroz, V. Kapila, and Q. Yan, “Adaptive nonlinear control of multiple spacecraft formation flying,” Journal of Guidance, Control, and Dynamics, vol. 23, no. 3, pp. 385–390, 2000. View at Publisher · View at Google Scholar · View at Scopus
  4. J. Georgie and J. Valasek, “Evaluation of longitudinal desired dynamics for dynamic-inversion controlled generic reentry vehicles,” Journal of Guidance, Control, and Dynamics, vol. 26, no. 5, pp. 811–819, 2003. View at Publisher · View at Google Scholar · View at Scopus
  5. D. Ito, J. Georgie, J. Valasek, and D. T. Ward, Reentry Vehicle Flight Controls Design Guidelines: Dynamic Inversion, NASA/TP—2002–210771, 2002.
  6. A. J. Ostroff and B. J. Bacon, “Force and moment approach for achievable dynamics using nonlinear dynamic inversion,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, pp. 424–434, Reston, Va, USA, 1999. View at Publisher · View at Google Scholar
  7. D. Enns, D. Bugajski, R. Hendrick, and G. Stein, “Dynamic inversion: an evolving methodology for flight control design,” International Journal of Control, vol. 59, no. 1, pp. 71–91, 1994. View at Google Scholar
  8. J. A. Richard, J. M. Buffington, A. G. Sparks, and S. S. Banda, Robust Multivariable Flight Control, Springer, New York, NY, USA, 1994.
  9. R. J. Adams and S. S. Banda, “Robust flight control design using dynamic inversion and structured singular value synthesis,” IEEE Transactions on Control Systems Technology, vol. 1, no. 2, pp. 80–92, 1993. View at Publisher · View at Google Scholar · View at Scopus
  10. M. B. McFarland and S. M. Hoque, “Robustness of a nonlinear missile autopilot designed using dynamic inversion,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA-2000-3970, Denver, Colo, USA, August 2000. View at Publisher · View at Google Scholar
  11. G. Looye and H.-D. Joos, “Design of robust dynamic inversion control laws using multi-objective optimization,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA-2001-4285, 2001. View at Publisher · View at Google Scholar
  12. P. B. Acquatella, W. Falkena, E. van Kampen, and Q. P. Chu, “Robust nonlinear spacecraft attitude control using incremental nonlinear dynamic inversion,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Minneapolis, Minn, USA, August 2012. View at Publisher · View at Google Scholar · View at Scopus
  13. P. K. Menon, V. R. Iragavarapu, and E. J. Ohlmeyer, “Nonlinear Missile Autopilot Design using Time-Scale Separation,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA-1997-3765, 1997. View at Publisher · View at Google Scholar
  14. A. Steinicke and G. Michalka, “Improving transient performance of dynamic inversion missile autopilot by use of backstepping,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA-2002-4658, Monterey, Calif, USA, August 2002. View at Publisher · View at Google Scholar
  15. I. Yang, D. Kim, and D. Lee, “A flight control strategy using robust dynamic inversion based on sliding mode control,” in proceeding of the AIAA Guidance, Navigation, and Control Conference, August 2012. View at Publisher · View at Google Scholar · View at Scopus
  16. H. Sira-Ramirez, “Differential geometric methods in variable-structure control,” International Journal of Control, vol. 48, no. 4, pp. 1359–1390, 1988. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus
  17. V. I. Utkin, “Variable structure systems with sliding modes,” IEEE Transactions on Automatic Control, vol. 22, no. 2, pp. 212–222, 1977. View at Google Scholar · View at MathSciNet · View at Scopus
  18. R. A. DeCarlo, S. H. Zak, and G. P. Matthews, “Variable structure control of nonlinear multivariable systems: a tutorial,” Proceedings of the IEEE, vol. 76, no. 3, pp. 212–232, 1988. View at Publisher · View at Google Scholar · View at Scopus
  19. J. Y. Hung, W. Gao, and J. C. Hung, “Variable structure control: a survey,” IEEE Transactions on Industrial Electronics, vol. 40, no. 1, pp. 2–22, 1993. View at Publisher · View at Google Scholar · View at Scopus
  20. G. Papageorgiou and M. Polansky, “Tuning a dynamic inversion pitch axis autopilot using McFarlane-Glover loop shaping,” Optimal Control Applications & Methods, vol. 30, no. 3, pp. 287–308, 2009. View at Publisher · View at Google Scholar · View at MathSciNet · View at Scopus