Adaptive fault tolerant attitude control of a stratospheric airship with input saturation

Zhaoxin Liang; Zewei Zheng; Ming Zhu; Zhe Wu

doi:10.1109/ICCA.2017.8003101

Adaptive fault tolerant attitude control of a stratospheric airship with input saturation

Zhaoxin Liang
, Zewei Zheng
, Ming Zhu
, Zhe Wu

Beihang University

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

3 Scopus citations

Abstract

In this work, an adaptive fault tolerant control method is proposed to address the problem of attitude tracking for stratospheric airship with both multiplicative and additive actuator faults. Input saturation for control surfaces are also considered and an auxiliary system is designed to deal with the saturation. Both multiplicative and additive actuator faults are estimated by a specific adaption law. Stability analysis, which is based on the Lyapunov stability theorem, shows that under the proposed control system, the estimate errors of actuator faults are bounded during operations. Simulations on a stratospheric airship attitude tracking control are presented to illustrate the effectiveness of the designed algorithm.

Original language	English
Title of host publication	2017 13th IEEE International Conference on Control and Automation, ICCA 2017
Publisher	IEEE Computer Society
Pages	443-448
Number of pages	6
ISBN (Electronic)	9781538626795
DOIs	https://doi.org/10.1109/ICCA.2017.8003101
State	Published - 4 Aug 2017
Event	13th IEEE International Conference on Control and Automation, ICCA 2017 - Ohrid, Macedonia, The Former Yugoslav Republic of Duration: 3 Jul 2017 → 6 Jul 2017

Publication series

Name	IEEE International Conference on Control and Automation, ICCA
ISSN (Print)	1948-3449
ISSN (Electronic)	1948-3457

Conference

Conference	13th IEEE International Conference on Control and Automation, ICCA 2017
Country/Territory	Macedonia, The Former Yugoslav Republic of
City	Ohrid
Period	3/07/17 → 6/07/17

Access to Document

10.1109/ICCA.2017.8003101

Cite this

Liang, Z., Zheng, Z., Zhu, M., & Wu, Z. (2017). Adaptive fault tolerant attitude control of a stratospheric airship with input saturation. In 2017 13th IEEE International Conference on Control and Automation, ICCA 2017 (pp. 443-448). Article 8003101 (IEEE International Conference on Control and Automation, ICCA). IEEE Computer Society. https://doi.org/10.1109/ICCA.2017.8003101

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title = "Adaptive fault tolerant attitude control of a stratospheric airship with input saturation",

abstract = "In this work, an adaptive fault tolerant control method is proposed to address the problem of attitude tracking for stratospheric airship with both multiplicative and additive actuator faults. Input saturation for control surfaces are also considered and an auxiliary system is designed to deal with the saturation. Both multiplicative and additive actuator faults are estimated by a specific adaption law. Stability analysis, which is based on the Lyapunov stability theorem, shows that under the proposed control system, the estimate errors of actuator faults are bounded during operations. Simulations on a stratospheric airship attitude tracking control are presented to illustrate the effectiveness of the designed algorithm.",

author = "Zhaoxin Liang and Zewei Zheng and Ming Zhu and Zhe Wu",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 13th IEEE International Conference on Control and Automation, ICCA 2017 ; Conference date: 03-07-2017 Through 06-07-2017",

year = "2017",

month = aug,

day = "4",

doi = "10.1109/ICCA.2017.8003101",

language = "英语",

series = "IEEE International Conference on Control and Automation, ICCA",

publisher = "IEEE Computer Society",

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booktitle = "2017 13th IEEE International Conference on Control and Automation, ICCA 2017",

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Liang, Z, Zheng, Z , Zhu, M & Wu, Z 2017, Adaptive fault tolerant attitude control of a stratospheric airship with input saturation. in 2017 13th IEEE International Conference on Control and Automation, ICCA 2017., 8003101, IEEE International Conference on Control and Automation, ICCA, IEEE Computer Society, pp. 443-448, 13th IEEE International Conference on Control and Automation, ICCA 2017, Ohrid, Macedonia, The Former Yugoslav Republic of, 3/07/17. https://doi.org/10.1109/ICCA.2017.8003101

Adaptive fault tolerant attitude control of a stratospheric airship with input saturation. / Liang, Zhaoxin; Zheng, Zewei ; Zhu, Ming et al.
2017 13th IEEE International Conference on Control and Automation, ICCA 2017. IEEE Computer Society, 2017. p. 443-448 8003101 (IEEE International Conference on Control and Automation, ICCA).

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

TY - GEN

T1 - Adaptive fault tolerant attitude control of a stratospheric airship with input saturation

AU - Liang, Zhaoxin

AU - Zheng, Zewei

AU - Zhu, Ming

AU - Wu, Zhe

PY - 2017/8/4

Y1 - 2017/8/4

N2 - In this work, an adaptive fault tolerant control method is proposed to address the problem of attitude tracking for stratospheric airship with both multiplicative and additive actuator faults. Input saturation for control surfaces are also considered and an auxiliary system is designed to deal with the saturation. Both multiplicative and additive actuator faults are estimated by a specific adaption law. Stability analysis, which is based on the Lyapunov stability theorem, shows that under the proposed control system, the estimate errors of actuator faults are bounded during operations. Simulations on a stratospheric airship attitude tracking control are presented to illustrate the effectiveness of the designed algorithm.

AB - In this work, an adaptive fault tolerant control method is proposed to address the problem of attitude tracking for stratospheric airship with both multiplicative and additive actuator faults. Input saturation for control surfaces are also considered and an auxiliary system is designed to deal with the saturation. Both multiplicative and additive actuator faults are estimated by a specific adaption law. Stability analysis, which is based on the Lyapunov stability theorem, shows that under the proposed control system, the estimate errors of actuator faults are bounded during operations. Simulations on a stratospheric airship attitude tracking control are presented to illustrate the effectiveness of the designed algorithm.

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DO - 10.1109/ICCA.2017.8003101

M3 - 会议稿件

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T3 - IEEE International Conference on Control and Automation, ICCA

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EP - 448

BT - 2017 13th IEEE International Conference on Control and Automation, ICCA 2017

PB - IEEE Computer Society

T2 - 13th IEEE International Conference on Control and Automation, ICCA 2017

Y2 - 3 July 2017 through 6 July 2017

ER -

Adaptive fault tolerant attitude control of a stratospheric airship with input saturation

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