Attitude control of flexible space structures using extended state observer

Authors

  • Bagus Mahawan Dynax Corporation
    Japan
  • Zheng-Hua Luo Dynaservo Inc.
    Canada
  • Jing-Qing Han Chinese Academy of Sciences
    China

Keywords:

attitude control, extended state observer, flexible satellites

Abstract

In this paper, we construct a nonlinear Extended State Observer (ESO) to estimate the dynamics of linear or nonlinear systems with parameter uncertainties and unknown external disturbances. We then apply ESO to the high-precision attitude control of a flexible satellite whose dynamics are unknown. Simulation results demonstrate the usefulness of the proposed control method.

References

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[2] Y. Chida, Y. Yamaguchi, H. Soga, T. Kida, I. Yamaguchi, T. Sekiguchi. On-orbit attitude control experiments for ETS-V1. Proc. of the 35 Conference on Decision and Control, Kobe, Japan, 486-488, 1996.
[3] Y. Chida, T. Kida, T. Sekiguchi. Attitude control experiments of ETS-VI using I-PD and two-degree-of-freedom H∞ control (in Japanese) . Journal of Systems, Control, and Information, 42(11): 591- 598, 1998.
[4] J.Q. Han. Auto disturbance rejection controller. Proc. of 2nd Asian Control Conference, Seoul, III: 567- 570, 1997.
[5] H. K. Khalil. Nonlinear Systems. Prentice Hall, New Jersey, 1996.

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Published

2023-03-01

Issue

pp. 501-512

Section

Articles

How to Cite

Mahawan, B., Luo, Z.-H., & Han, J.-Q. (2023). Attitude control of flexible space structures using extended state observer. Computer Assisted Methods in Engineering and Science, 8(4), 501-512. https://cames3.ippt.pan.pl/index.php/cames/article/view/1154