STATE-DEPENDENT BOUNDARY LAYER METHOD FOR ATTITUDE CONTROL OF SATELLITE

Authors

  • Nurul Syazwani Hussain School of Mechatronic Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Hassrizal Hasan Basri School of Mechatronic Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Sazali Yaacob Universiti Kuala Lumpur Malaysian Spanish Institute, Kulim Hi-TechPark, 09000 Kulim, Kedah, Malaysia

DOI:

https://doi.org/10.11113/jt.v76.5885

Keywords:

Sliding mode control, mathematical model, attitude control, state dependant boundary layer

Abstract

Sliding mode control is known to be robust against parameter uncertainties and external disturbances. Based on the dynamic equation of motion, a sliding mode controller is designed to solve this problem. However, for the sliding surface to be attractive, a switching function is used in the control law, which caused chattering of the control signal. In order to avoid this, a boundary layer method is considered in the modified controller. So this paper proposes new boundary layer designs that resolve the problem in control accuracy and control signal smoothness in sliding mode control. The propose design improve the system state to almost zero with no chattering in the control signals.

References

M. J. Sidi. 2000. Spacecraft Dynamics and Control: A Practical Engineering Approach. Cambridge University Press,

Min-Shin Chen, Yean-Ren Hwang and Masayoshi Tomizuka. 2002. A State Dependent Boundary Layer Design for Sliding Mode Control. IEEE Transactions on Automatic Control. 47(10).

C. D. Richard, H. B. Robert. 2011. Modern Control System. New Jersey: Pearson Education Inc.,

Jong Hyu Lee, Chan Gook Park, Heung Won Park. 1993. Sliding Mode Controller Design for Spacecraft Attitude Tracking Maneuves.

Hyng-Chul Lim, Hyo-Choong Bang, Kwan-Dong Park, Phil-Do Park. 2003. Tracking Control Design Using Sliding Mode Techniques for Satellite Formation Flying.

Hakan Elmali and NejatOlgac. 1991. Robust Tracking Control of Nonlinear MIMO systems via Sliding Mode Control.

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Published

2015-10-13

Issue

Vol. 76 No. 12: Man-Machine Systems

Section

Science and Engineering

License

Copyright of articles that appear in Jurnal Teknologi belongs exclusively to Penerbit Universiti Teknologi Malaysia (Penerbit UTM Press). This copyright covers the rights to reproduce the article, including reprints, electronic reproductions, or any other reproductions of similar nature.

How to Cite

STATE-DEPENDENT BOUNDARY LAYER METHOD FOR ATTITUDE CONTROL OF SATELLITE. (2015). Jurnal Teknologi, 76(12). https://doi.org/10.11113/jt.v76.5885