Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck

Haibo Ji; Lei Wang; Zhuoyue Song; Xiangdong Liu; Zhirong Lei

doi:10.23919/ChiCC.2017.8027473

Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck

Haibo Ji, Lei Wang, Zhuoyue Song^*, Xiangdong Liu, Zhirong Lei

^*Corresponding author for this work

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

Abstract

This paper presents nonlinear robust trajectory tracking strategies for the hypersonic vehicle whose ailerons are stuck at an unknown angular position. Firstly, a time-varying sliding mode control strategy for general second-order systems is introduced, and the chattering of sliding mode controller is alleviated. Secondly, the dynamics of hypersonic vehicle are transformed into two second-order systems. Then, the corresponding guidance law and attitude controller are designed using time-varying sliding mode controller. By the proposed strategies, the hypersonic vehicle can fly along the reference trajectory. Finally, the proposed strategies are applied to a hypersonic platform to verify its validity.

Original language	English
Title of host publication	Proceedings of the 36th Chinese Control Conference, CCC 2017
Editors	Tao Liu, Qianchuan Zhao
Publisher	IEEE Computer Society
Pages	985-989
Number of pages	5
ISBN (Electronic)	9789881563934
DOIs	https://doi.org/10.23919/ChiCC.2017.8027473
Publication status	Published - 7 Sept 2017
Event	36th Chinese Control Conference, CCC 2017 - Dalian, China Duration: 26 Jul 2017 → 28 Jul 2017

Publication series

Name	Chinese Control Conference, CCC
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	36th Chinese Control Conference, CCC 2017
Country/Territory	China
City	Dalian
Period	26/07/17 → 28/07/17

Keywords

Stuck Aileron
Time-Varying Sliding Mode
Trajectory Tracking

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10.23919/ChiCC.2017.8027473

Cite this

Ji, H., Wang, L., Song, Z., Liu, X., & Lei, Z. (2017). Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck. In T. Liu, & Q. Zhao (Eds.), Proceedings of the 36th Chinese Control Conference, CCC 2017 (pp. 985-989). Article 8027473 (Chinese Control Conference, CCC). IEEE Computer Society. https://doi.org/10.23919/ChiCC.2017.8027473

@inproceedings{7a92c707c6a544b9b315c1b50e936a79,

title = "Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck",

abstract = "This paper presents nonlinear robust trajectory tracking strategies for the hypersonic vehicle whose ailerons are stuck at an unknown angular position. Firstly, a time-varying sliding mode control strategy for general second-order systems is introduced, and the chattering of sliding mode controller is alleviated. Secondly, the dynamics of hypersonic vehicle are transformed into two second-order systems. Then, the corresponding guidance law and attitude controller are designed using time-varying sliding mode controller. By the proposed strategies, the hypersonic vehicle can fly along the reference trajectory. Finally, the proposed strategies are applied to a hypersonic platform to verify its validity.",

keywords = "Stuck Aileron, Time-Varying Sliding Mode, Trajectory Tracking",

author = "Haibo Ji and Lei Wang and Zhuoyue Song and Xiangdong Liu and Zhirong Lei",

note = "Publisher Copyright: {\textcopyright} 2017 Technical Committee on Control Theory, CAA.; 36th Chinese Control Conference, CCC 2017 ; Conference date: 26-07-2017 Through 28-07-2017",

year = "2017",

month = sep,

day = "7",

doi = "10.23919/ChiCC.2017.8027473",

language = "English",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "985--989",

editor = "Tao Liu and Qianchuan Zhao",

booktitle = "Proceedings of the 36th Chinese Control Conference, CCC 2017",

address = "United States",

}

Ji, H, Wang, L, Song, Z, Liu, X & Lei, Z 2017, Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck. in T Liu & Q Zhao (eds), Proceedings of the 36th Chinese Control Conference, CCC 2017., 8027473, Chinese Control Conference, CCC, IEEE Computer Society, pp. 985-989, 36th Chinese Control Conference, CCC 2017, Dalian, China, 26/07/17. https://doi.org/10.23919/ChiCC.2017.8027473

Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck. / Ji, Haibo; Wang, Lei; Song, Zhuoyue et al.
Proceedings of the 36th Chinese Control Conference, CCC 2017. ed. / Tao Liu; Qianchuan Zhao. IEEE Computer Society, 2017. p. 985-989 8027473 (Chinese Control Conference, CCC).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck

AU - Ji, Haibo

AU - Wang, Lei

AU - Song, Zhuoyue

AU - Liu, Xiangdong

AU - Lei, Zhirong

PY - 2017/9/7

Y1 - 2017/9/7

N2 - This paper presents nonlinear robust trajectory tracking strategies for the hypersonic vehicle whose ailerons are stuck at an unknown angular position. Firstly, a time-varying sliding mode control strategy for general second-order systems is introduced, and the chattering of sliding mode controller is alleviated. Secondly, the dynamics of hypersonic vehicle are transformed into two second-order systems. Then, the corresponding guidance law and attitude controller are designed using time-varying sliding mode controller. By the proposed strategies, the hypersonic vehicle can fly along the reference trajectory. Finally, the proposed strategies are applied to a hypersonic platform to verify its validity.

AB - This paper presents nonlinear robust trajectory tracking strategies for the hypersonic vehicle whose ailerons are stuck at an unknown angular position. Firstly, a time-varying sliding mode control strategy for general second-order systems is introduced, and the chattering of sliding mode controller is alleviated. Secondly, the dynamics of hypersonic vehicle are transformed into two second-order systems. Then, the corresponding guidance law and attitude controller are designed using time-varying sliding mode controller. By the proposed strategies, the hypersonic vehicle can fly along the reference trajectory. Finally, the proposed strategies are applied to a hypersonic platform to verify its validity.

KW - Stuck Aileron

KW - Time-Varying Sliding Mode

KW - Trajectory Tracking

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DO - 10.23919/ChiCC.2017.8027473

M3 - Conference contribution

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T3 - Chinese Control Conference, CCC

SP - 985

EP - 989

BT - Proceedings of the 36th Chinese Control Conference, CCC 2017

A2 - Liu, Tao

A2 - Zhao, Qianchuan

PB - IEEE Computer Society

T2 - 36th Chinese Control Conference, CCC 2017

Y2 - 26 July 2017 through 28 July 2017

ER -

Trajectory tracking based on time-varying sliding mode controller for hypersonic vehicle with aileron stuck

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