Anti-disturbance PD controller design for flexible spacecraft attitude stabilization

Eddine Benmansour Jalal; Yijiang Du; Zhong Wu

doi:10.1109/ChiCC.2015.7260527

Anti-disturbance PD controller design for flexible spacecraft attitude stabilization

Eddine Benmansour Jalal
, Yijiang Du
, Zhong Wu

School of Instrumentation and Optoelectronic Engineering

Beihang University

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

9 Scopus citations

Abstract

Both vibrations and model uncertainties will pose great challenges for accurate attitude control of flexible spacecrafts. In this paper, an anti-disturbance proportional-derivative (PD) controller is designed to stabilize the attitude while rejecting the effects of flexible vibrations, environmental disturbances, and unmodeled dynamics, which are assumed as an extended state. This controller comprises two parts, i.e. an extended state observer and a PD controller with feedforward. First, flexible vibrations, environmental disturbances, and unmodeled dynamics are regarded as an extended state which can be estimated by the extended state observer. Then, the estimated extended state can be compensated by feedforward and the attitude can be stabilized by the PD controller. Numerical simulation results are presented to demonstrate the effectiveness of the control scheme.

Original language	English
Title of host publication	Proceedings of the 34th Chinese Control Conference, CCC 2015
Editors	Qianchuan Zhao, Shirong Liu
Publisher	IEEE Computer Society
Pages	5687-5690
Number of pages	4
ISBN (Electronic)	9789881563897
DOIs	https://doi.org/10.1109/ChiCC.2015.7260527
State	Published - 11 Sep 2015
Event	34th Chinese Control Conference, CCC 2015 - Hangzhou, China Duration: 28 Jul 2015 → 30 Jul 2015

Publication series

Name	Chinese Control Conference, CCC
Volume	2015-September
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	34th Chinese Control Conference, CCC 2015
Country/Territory	China
City	Hangzhou
Period	28/07/15 → 30/07/15

Keywords

Attitude Stabilization
Extended State Observer
Flexible Spacecraft
Proportional-Derivative Control

Access to Document

10.1109/ChiCC.2015.7260527

Cite this

Benmansour Jalal, E., Du, Y., & Wu, Z. (2015). Anti-disturbance PD controller design for flexible spacecraft attitude stabilization. In Q. Zhao, & S. Liu (Eds.), Proceedings of the 34th Chinese Control Conference, CCC 2015 (pp. 5687-5690). Article 7260527 (Chinese Control Conference, CCC; Vol. 2015-September). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2015.7260527

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title = "Anti-disturbance PD controller design for flexible spacecraft attitude stabilization",

abstract = "Both vibrations and model uncertainties will pose great challenges for accurate attitude control of flexible spacecrafts. In this paper, an anti-disturbance proportional-derivative (PD) controller is designed to stabilize the attitude while rejecting the effects of flexible vibrations, environmental disturbances, and unmodeled dynamics, which are assumed as an extended state. This controller comprises two parts, i.e. an extended state observer and a PD controller with feedforward. First, flexible vibrations, environmental disturbances, and unmodeled dynamics are regarded as an extended state which can be estimated by the extended state observer. Then, the estimated extended state can be compensated by feedforward and the attitude can be stabilized by the PD controller. Numerical simulation results are presented to demonstrate the effectiveness of the control scheme.",

keywords = "Attitude Stabilization, Extended State Observer, Flexible Spacecraft, Proportional-Derivative Control",

author = "\{Benmansour Jalal\}, Eddine and Yijiang Du and Zhong Wu",

note = "Publisher Copyright: {\textcopyright} 2015 Technical Committee on Control Theory, Chinese Association of Automation.; 34th Chinese Control Conference, CCC 2015 ; Conference date: 28-07-2015 Through 30-07-2015",

year = "2015",

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day = "11",

doi = "10.1109/ChiCC.2015.7260527",

language = "英语",

series = "Chinese Control Conference, CCC",

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Benmansour Jalal, E, Du, Y & Wu, Z 2015, Anti-disturbance PD controller design for flexible spacecraft attitude stabilization. in Q Zhao & S Liu (eds), Proceedings of the 34th Chinese Control Conference, CCC 2015., 7260527, Chinese Control Conference, CCC, vol. 2015-September, IEEE Computer Society, pp. 5687-5690, 34th Chinese Control Conference, CCC 2015, Hangzhou, China, 28/07/15. https://doi.org/10.1109/ChiCC.2015.7260527

Anti-disturbance PD controller design for flexible spacecraft attitude stabilization. / Benmansour Jalal, Eddine; Du, Yijiang; Wu, Zhong.
Proceedings of the 34th Chinese Control Conference, CCC 2015. ed. / Qianchuan Zhao; Shirong Liu. IEEE Computer Society, 2015. p. 5687-5690 7260527 (Chinese Control Conference, CCC; Vol. 2015-September).

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

TY - GEN

T1 - Anti-disturbance PD controller design for flexible spacecraft attitude stabilization

AU - Benmansour Jalal, Eddine

AU - Du, Yijiang

AU - Wu, Zhong

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N2 - Both vibrations and model uncertainties will pose great challenges for accurate attitude control of flexible spacecrafts. In this paper, an anti-disturbance proportional-derivative (PD) controller is designed to stabilize the attitude while rejecting the effects of flexible vibrations, environmental disturbances, and unmodeled dynamics, which are assumed as an extended state. This controller comprises two parts, i.e. an extended state observer and a PD controller with feedforward. First, flexible vibrations, environmental disturbances, and unmodeled dynamics are regarded as an extended state which can be estimated by the extended state observer. Then, the estimated extended state can be compensated by feedforward and the attitude can be stabilized by the PD controller. Numerical simulation results are presented to demonstrate the effectiveness of the control scheme.

AB - Both vibrations and model uncertainties will pose great challenges for accurate attitude control of flexible spacecrafts. In this paper, an anti-disturbance proportional-derivative (PD) controller is designed to stabilize the attitude while rejecting the effects of flexible vibrations, environmental disturbances, and unmodeled dynamics, which are assumed as an extended state. This controller comprises two parts, i.e. an extended state observer and a PD controller with feedforward. First, flexible vibrations, environmental disturbances, and unmodeled dynamics are regarded as an extended state which can be estimated by the extended state observer. Then, the estimated extended state can be compensated by feedforward and the attitude can be stabilized by the PD controller. Numerical simulation results are presented to demonstrate the effectiveness of the control scheme.

KW - Attitude Stabilization

KW - Extended State Observer

KW - Flexible Spacecraft

KW - Proportional-Derivative Control

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ER -

Anti-disturbance PD controller design for flexible spacecraft attitude stabilization

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