Sliding Mode Control for Spacecraft Large Angel Attitude Control with Fuel Sloshing

Xiao Juan Song; Bao Zeng Yue

doi:10.4028/www.scientific.net/AMM.670-671.683

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 670-671Sliding Mode Control for Spacecraft Large Angel...

Sliding Mode Control for Spacecraft Large Angel Attitude Control with Fuel Sloshing

Abstract:

This paper presents the analysis of the spacecraft with fuel sloshing during attitude maneuver. The fuzzy sliding mode controller is designed for a simplified model of the spacecraft. The controller includes an equivalent control term, a sliding controller, and an optimal controller by adaptive fuzzy algorithm for perturbation parameters. Extensively numerical simulations are carried to verify effect of the control method in this paper and the numerical results show the good performance and better effectiveness for the fuel-filled spacecraft large attitude maneuver.

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Periodical:

Applied Mechanics and Materials (Volumes 670-671)

Pages:

683-686

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.670-671.683

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Cite this paper

Online since:

October 2014

Authors:

Xiao Juan Song*, Bao Zeng Yue

Keywords:

Adaptive Fuzzy Sliding Mode Controller, Fuel Sloshing, Fuel-Filled Spacecraft

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* - Corresponding Author

References

[1] H. Shageer, and G. Tao. Modeling and adaptive control of spacecraft with fuel slosh: overview and case studies. in AIAA Guidance, Navigation, and Control Conference, Hiton Head, South Carolina. (2007).

DOI: 10.2514/6.2007-6434

Google Scholar

[2] N. Qi, and K. Dong, et al. Spacecraft propellant sloshing suppression using input shaping technique. in Computer Modeling and Simulation, 2009. ICCMS 2009 IEEE.

DOI: 10.1109/iccms.2009.20

Google Scholar

[3] B. Yue, L. Zhu. Hybrid control of liquid-filled spacecraft maneuvers by dynamic inversion and input shaping[J]. AIAA Journal. 2014: 1-9.

DOI: 10.2514/1.j052526

Google Scholar

[4] M. Reyhanoglu, and J.R. Hervas, Robotically controlled sloshing suppression in point-to-point liquid container transfer. Journal of Vibration and Control, 2013. 19(14): pp.2137-2144.

DOI: 10.1177/1077546312456865

Google Scholar

[5] M. Reyhanoglu, and J.R. Hervas, Nonlinear dynamics and control of space vehicles with multiple fuel slosh modes. Control Engineering Practice, 2012. 20(9): pp.912-918.

DOI: 10.1016/j.conengprac.2012.05.011

Google Scholar