Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer

Juan Dai; Yuanqing Xia

doi:10.1109/ICIT.2016.7475036

Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer

Juan Dai, Yuanqing Xia

School of Automation

Beijing Institute of Technology

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

3 Citations (Scopus)

Abstract

In this paper, the finite-time trajectory tracking control problem for Mars landing with disturbances is addressed. To improve the accuracy of Mars landing, a new nonlinear entry guidance law for low lift landers has been developed. The sliding mode control (SMC) compound with extended state observer (ESO) for tracking a reference trajectory is proposed. The guidance method is based on SMC theory and ESO adapted to the problem of entry guidance. ESO are applied to estimate the disturbance, by which sliding mode controller is designed combining the two approaches respectively to force the state variables of the closed loop system to converge to the reference trajectory. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

Original language	English
Title of host publication	Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1796-1801
Number of pages	6
ISBN (Electronic)	9781467380751
DOIs	https://doi.org/10.1109/ICIT.2016.7475036
Publication status	Published - 19 May 2016
Event	IEEE International Conference on Industrial Technology, ICIT 2016 - Taipei, Taiwan, Province of China Duration: 14 Mar 2016 → 17 Mar 2016

Publication series

Name	Proceedings of the IEEE International Conference on Industrial Technology
Volume	2016-May

Conference

Conference	IEEE International Conference on Industrial Technology, ICIT 2016
Country/Territory	Taiwan, Province of China
City	Taipei
Period	14/03/16 → 17/03/16

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10.1109/ICIT.2016.7475036

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Dai, J., & Xia, Y. (2016). Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer. In Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016 (pp. 1796-1801). Article 7475036 (Proceedings of the IEEE International Conference on Industrial Technology; Vol. 2016-May). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICIT.2016.7475036

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title = "Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer",

abstract = "In this paper, the finite-time trajectory tracking control problem for Mars landing with disturbances is addressed. To improve the accuracy of Mars landing, a new nonlinear entry guidance law for low lift landers has been developed. The sliding mode control (SMC) compound with extended state observer (ESO) for tracking a reference trajectory is proposed. The guidance method is based on SMC theory and ESO adapted to the problem of entry guidance. ESO are applied to estimate the disturbance, by which sliding mode controller is designed combining the two approaches respectively to force the state variables of the closed loop system to converge to the reference trajectory. Also, simulation results are presented to illustrate the effectiveness of the control strategy.",

author = "Juan Dai and Yuanqing Xia",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; IEEE International Conference on Industrial Technology, ICIT 2016 ; Conference date: 14-03-2016 Through 17-03-2016",

year = "2016",

month = may,

day = "19",

doi = "10.1109/ICIT.2016.7475036",

language = "English",

series = "Proceedings of the IEEE International Conference on Industrial Technology",

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Dai, J & Xia, Y 2016, Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer. in Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016., 7475036, Proceedings of the IEEE International Conference on Industrial Technology, vol. 2016-May, Institute of Electrical and Electronics Engineers Inc., pp. 1796-1801, IEEE International Conference on Industrial Technology, ICIT 2016, Taipei, Taiwan, Province of China, 14/03/16. https://doi.org/10.1109/ICIT.2016.7475036

Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer. / Dai, Juan; Xia, Yuanqing.
Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016. Institute of Electrical and Electronics Engineers Inc., 2016. p. 1796-1801 7475036 (Proceedings of the IEEE International Conference on Industrial Technology; Vol. 2016-May).

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

TY - GEN

T1 - Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer

AU - Dai, Juan

AU - Xia, Yuanqing

PY - 2016/5/19

Y1 - 2016/5/19

N2 - In this paper, the finite-time trajectory tracking control problem for Mars landing with disturbances is addressed. To improve the accuracy of Mars landing, a new nonlinear entry guidance law for low lift landers has been developed. The sliding mode control (SMC) compound with extended state observer (ESO) for tracking a reference trajectory is proposed. The guidance method is based on SMC theory and ESO adapted to the problem of entry guidance. ESO are applied to estimate the disturbance, by which sliding mode controller is designed combining the two approaches respectively to force the state variables of the closed loop system to converge to the reference trajectory. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

AB - In this paper, the finite-time trajectory tracking control problem for Mars landing with disturbances is addressed. To improve the accuracy of Mars landing, a new nonlinear entry guidance law for low lift landers has been developed. The sliding mode control (SMC) compound with extended state observer (ESO) for tracking a reference trajectory is proposed. The guidance method is based on SMC theory and ESO adapted to the problem of entry guidance. ESO are applied to estimate the disturbance, by which sliding mode controller is designed combining the two approaches respectively to force the state variables of the closed loop system to converge to the reference trajectory. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

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DO - 10.1109/ICIT.2016.7475036

M3 - Conference contribution

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T3 - Proceedings of the IEEE International Conference on Industrial Technology

SP - 1796

EP - 1801

BT - Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - IEEE International Conference on Industrial Technology, ICIT 2016

Y2 - 14 March 2016 through 17 March 2016

ER -

Dai J, Xia Y. Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer. In Proceedings - 2016 IEEE International Conference on Industrial Technology, ICIT 2016. Institute of Electrical and Electronics Engineers Inc. 2016. p. 1796-1801. 7475036. (Proceedings of the IEEE International Conference on Industrial Technology). doi: 10.1109/ICIT.2016.7475036

Sliding mode trajectory tracking for mars atmospheric entry based on extended state observer

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