Second order sliding mode control with backstepping approach for moving mass spinning missiles

Peng Fei Guo; Shu Xing Yang; Liang Yu Zhao

doi:10.15918/j.jbit1004-0579.201625.0103

Second order sliding mode control with backstepping approach for moving mass spinning missiles

Peng Fei Guo, Shu Xing Yang, Liang Yu Zhao^*

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

1 Citation (Scopus)

Abstract

An attitude controller using the second order sliding mode control methodology with a backstepping approach (SOSMCB) is designed and implemented for a spinning missile with two internal moving mass blocks. The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics. The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach, and its stability is proved by means of a Lyapunov function. The performance of the controller is demonstrated by numerical simulations, the results show that the attitude controller is stable and effective.

Original language	English
Pages (from-to)	17-22
Number of pages	6
Journal	Journal of Beijing Institute of Technology (English Edition)
Volume	25
Issue number	1
DOIs	https://doi.org/10.15918/j.jbit1004-0579.201625.0103
Publication status	Published - 1 Mar 2016

Keywords

Backstepping
Moving mass
Second order sliding mode control
Spinning missile

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10.15918/j.jbit1004-0579.201625.0103

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title = "Second order sliding mode control with backstepping approach for moving mass spinning missiles",

abstract = "An attitude controller using the second order sliding mode control methodology with a backstepping approach (SOSMCB) is designed and implemented for a spinning missile with two internal moving mass blocks. The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics. The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach, and its stability is proved by means of a Lyapunov function. The performance of the controller is demonstrated by numerical simulations, the results show that the attitude controller is stable and effective.",

keywords = "Backstepping, Moving mass, Second order sliding mode control, Spinning missile",

author = "Guo, {Peng Fei} and Yang, {Shu Xing} and Zhao, {Liang Yu}",

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AU - Guo, Peng Fei

AU - Yang, Shu Xing

AU - Zhao, Liang Yu

PY - 2016/3/1

Y1 - 2016/3/1

N2 - An attitude controller using the second order sliding mode control methodology with a backstepping approach (SOSMCB) is designed and implemented for a spinning missile with two internal moving mass blocks. The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics. The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach, and its stability is proved by means of a Lyapunov function. The performance of the controller is demonstrated by numerical simulations, the results show that the attitude controller is stable and effective.

AB - An attitude controller using the second order sliding mode control methodology with a backstepping approach (SOSMCB) is designed and implemented for a spinning missile with two internal moving mass blocks. The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics. The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach, and its stability is proved by means of a Lyapunov function. The performance of the controller is demonstrated by numerical simulations, the results show that the attitude controller is stable and effective.

KW - Backstepping

KW - Moving mass

KW - Second order sliding mode control

KW - Spinning missile

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JO - Journal of Beijing Institute of Technology (English Edition)

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Second order sliding mode control with backstepping approach for moving mass spinning missiles

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Keywords

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