Paper Titles
Computer Control Software Design Model Based on Improved PID Algorithm
p.1671
Using Image Registration Method to Register UAV
p.1675
Study of the Time-Delay System with Integral-Type
p.1680
Analysis of the Reactive Power Control Strategy Based on Improved Particle Swarm Algorithm
p.1684
Flight Attitude Sliding Mode Control Design Based on the Compensation of Extended State Observer
p.1689
Fuzzy Nonsingular Terminal Sliding Mode Control for Attitude of Flapping Wing Micro Aerial Vehicle
p.1694
Temperature Optimal Control Model Design of the Metal Material Smelting
p.1699
Study on Application of Expert Systems in PID Thermostatic Control
p.1703
Research on the Cooling System of High-Speed Motorized Spindle
p.1707

Flight Attitude Sliding Mode Control Design Based on the Compensation of Extended State Observer

Article Preview

Abstract:

This paper proposes the sliding mode control design based on extended state observer control approch for the flight attitude system.The extended state observer (ESO) with new structure is used to estimate the total disturbance and to compensate the control object so that the flight attitude system can be simplified. Then a sliding mode controller is used to stabilize this simplified system. Finally, a numerical simulation shows the effectiveness of the proposed control design method.

You might also be interested in these eBooks
Mechanical Engineering and Materials Science View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 716-717)

Pages:

1689-1693

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.716-717.1689

Citation:

Cite this paper

Online since:

December 2014

Authors:

Hai Long Xing*, Juan Li

Keywords:

Extended State Observer, Sliding Mode Contro, Spacecraft Attitude Tracking

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

References

[1] Adams, R.J., Buffington, J. M., Sparks, A. G. and Banda, S. S. Robust Multivariable Flight Control, Springer-Verlag, (1994).

Google Scholar

[2] Blakelock, J.H. Automatic Control of Aircraft and Missiles, Wiley, New York, (1991).

Google Scholar

[3] Meyer, G., Su R. and Hunt L.R. Application of nonlinear transformations to automatic flight control[J]. Automatica, 1984, 20(1), 103-107.

DOI: 10.1016/0005-1098(84)90069-4

Google Scholar

[4] Lane, S.H. and Stengel, R.F. Flight control design using nonlinear inverse dynamics [J]. Automatica, 1988, 24(4), 471-483.

DOI: 10.1016/0005-1098(88)90092-1

Google Scholar

[5] Luo W, Chu Y C, Ling K V. H∞ actions inverse optimal attitude tracking control of rigid spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(3): 481- 493.

DOI: 10.2514/1.6471

Google Scholar

[6] Seo D, Akella M R. High-performance spacecraft adaptive attitude-tracking control through attracting manifold design[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 884-891.

DOI: 10.2514/1.33308

Google Scholar

[7] Jin Y, Liu X, Qiu W, et al. Time-varying sliding mode controls in rigid spacecraft attitude tracking[J]. Chinese Journal of Aeronautics, 2008, 21: 352-360.

DOI: 10.1016/s1000-9361(08)60046-1

Google Scholar

[8] Kim K S, Kim Y. Robust backstepping control for slew maneuver using nonlinear tracking function[J]. IEEE Transactions on Control System Technology, 2003, 11: 822-829.

DOI: 10.1109/tcst.2003.815608

Google Scholar

[9] Liu Y C, Zhang T, Liu B, et al. Controller design based on similar skew-symmetric structure[J]. Journal of Tsinghua University (Science and Technology), 2009, 49(7): 1047-1049. [in Chinese].

Google Scholar