Attitude Maneuver Control of Flexible Spacecraft with Finite-Time Convergence

Shu Nan Wu; Zhao Wei Sun; Xian De Wu

doi:10.4028/www.scientific.net/AMM.157-158.847

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 157-158Attitude Maneuver Control of Flexible Spacecraft...

Attitude Maneuver Control of Flexible Spacecraft with Finite-Time Convergence

Abstract:

The attitude maneuver control of flexible spacecraft with finite-time convergence is investigated in this paper. Two terminal sliding mode controllers are proposed to achieve the finite-time control, which guarantee the convergence of attitude maneuver errors in finite time. The singularity problem associated with the terminal sliding mode control is solved by employing a new sliding variable. Numerical simulations are finally provided to illustrate the performance of the proposed controllers.

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Periodical:

Applied Mechanics and Materials (Volumes 157-158)

Pages:

847-851

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.157-158.847

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Online since:

February 2012

Authors:

Shu Nan Wu, Zhao Wei Sun, Xian De Wu

Keywords:

Attitude Maneuver, Finite Time, Flexible Spacecraft, Terminal Sliding Mode Control

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References

[1] P.K.C. Wang, and F.Y. Hadaegh, Coordination and control of multiple microspacecraft moving in formation, The Journal of the Astronautical Sciences. 44 (1996) 315-355.

Google Scholar

[2] J.T-Y. Wen, and K. Kreutz-Delgado, The attitude control problem, IEEE Transactions on Automatic Control. 36 (1991) 1148-1161.

DOI: 10.1109/9.90228

Google Scholar

[3] R. Kristiansen, P.J. Nicklasson, and J.T. Gravdahl, Satellite attitude control by quaternion-based backstepping, IEEE Transactions on Control Systems Technology. 17 (2009) 227-232.

DOI: 10.1109/tcst.2008.924576

Google Scholar

[4] Y.G. Hong, Finite-time stabilization and stabilizability of a class of controllable systems, System and Control Letters. 46 (2002) 231-236.

DOI: 10.1016/s0167-6911(02)00119-6

Google Scholar

[5] E. Jin, and Z. Sun, Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control, Aerospace Science and Technology. 12 (2008) 324–330.

DOI: 10.1016/j.ast.2007.08.001

Google Scholar

[6] S. Wu, G. Radice, Y. Gao, and Z. Sun, Quaternion-based finite time control for spacecraft attitude tracking, Acta Astronautica. 69 (2011) 48–58.

DOI: 10.1016/j.actaastro.2011.03.001

Google Scholar

[7] E. Jin, and Z. Sun, Robust attitude tracking control of flexible spacecraft for achieving globally asymptotic stability, International Journal of Robust and Nonlinear Control. 19 (2009) 1201-1223.

DOI: 10.1002/rnc.1373

Google Scholar

[8] Y. Feng, X. Yu, and Z. Man, Non-singular terminal sliding mode control of rigid manipulators, Automatica. 38 (2002) 2159-2167.

DOI: 10.1016/s0005-1098(02)00147-4

Google Scholar