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

Hai Long Xing; Juan Li

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

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 716-717Flight Attitude Sliding Mode Control Design Based...

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

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.

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Periodical:

Applied Mechanics and Materials (Volumes 716-717)

Pages:

1689-1693

DOI:

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

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Online since:

December 2014

Authors:

Hai Long Xing*, Juan Li

Keywords:

Extended State Observer, Sliding Mode Contro, Spacecraft Attitude Tracking

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* - Corresponding Author

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