A Variable Structure Attitude Control System Design Based on Finite Time Stability

Rui Min Jiang; Jun Zhou; Jian Guo Guo

doi:10.4028/www.scientific.net/AMM.446-447.1141

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 446-447A Variable Structure Attitude Control System...

A Variable Structure Attitude Control System Design Based on Finite Time Stability

Abstract:

A variable structure attitude control system design method that guarantees the finite-time stability is proposed for hypersonic vehicle attitude control. According to the characteristics of the hypersonic vehicle longitudinal attitude model, it is considered to comprise attack angle control loop and angular rate control loop. The attack angle controller and pitch angular rate controller based on variable structure control are designed respectively which ensure the finite-time stability. The finite-time stability of the whole attitude control system has been proved .The simulation results illustrated that the proposed attitude controller has good rapidity and robustness.

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Periodical:

Applied Mechanics and Materials (Volumes 446-447)

Pages:

1141-1145

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.446-447.1141

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Online since:

November 2013

Authors:

Rui Min Jiang, Jun Zhou, Jian Guo Guo

Keywords:

Attitude Control, Finite Time Stability, Hypersonic Vehicle, Variable Structure Control

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