Sliding Variable Structure Control for Attitude of Moving-Mass Hypersonic Vehicles

Yu Kun Wang; Zhen Zhang; Jian Qin Mao

doi:10.4028/www.scientific.net/AMM.325-326.1225

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 325-326Sliding Variable Structure Control for Attitude of...

Sliding Variable Structure Control for Attitude of Moving-Mass Hypersonic Vehicles

Abstract:

The moving-mass hypersonic attitude dynamic model is a strong nonlinear, multivariable, and strong coupling system. Based on the reasonable assumption, a simplified dynamic model is given. According to the time-scale separation theory, a sliding variable structure controller is designed and implemented for the tracking control of angular velocity and angle at the same time. Simulation results demonstrate the effectiveness of controller.

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Periodical:

Applied Mechanics and Materials (Volumes 325-326)

Pages:

1225-1228

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.325-326.1225

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Online since:

June 2013

Authors:

Yu Kun Wang, Zhen Zhang, Jian Qin Mao

Keywords:

Attitude Control, Dynamic Inversion, Moving-Mass, Variable Structure Control (VSC)

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References

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