Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints

Zhijie Liu; Jinkun Liu; Lijun Wang

doi:10.1016/j.ast.2017.11.036

Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints

Zhijie Liu
, Jinkun Liu^*
, Lijun Wang

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
Key Laboratory of Precision Opto-Mechatronics Technology (Ministry of Education)

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

126 Scopus citations

Abstract

In this paper, we investigate the problem of attitude control design for flexible spacecraft with external disturbance, input magnitude and rate constraints. First, a disturbance observer is designed to estimate and compensate for the disturbances including the external disturbance and vibration from the flexible appendages. Then, based on the disturbance observer, a sample state feedback control scheme is proposed for flexible spacecraft subject to input magnitude and rate constrains, using the linear matrix inequality (LMI) and Lyapunov direct method. Finally, the results are illustrated using numerical simulations for control performance verification.

Original language	English
Pages (from-to)	486-492
Number of pages	7
Journal	Aerospace Science and Technology
Volume	72
DOIs	https://doi.org/10.1016/j.ast.2017.11.036
State	Published - Jan 2018

Keywords

Disturbance observer
Flexible spacecraft
Input magnitude and rate constraints
LMI technology
State feedback control

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10.1016/j.ast.2017.11.036

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title = "Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints",

abstract = "In this paper, we investigate the problem of attitude control design for flexible spacecraft with external disturbance, input magnitude and rate constraints. First, a disturbance observer is designed to estimate and compensate for the disturbances including the external disturbance and vibration from the flexible appendages. Then, based on the disturbance observer, a sample state feedback control scheme is proposed for flexible spacecraft subject to input magnitude and rate constrains, using the linear matrix inequality (LMI) and Lyapunov direct method. Finally, the results are illustrated using numerical simulations for control performance verification.",

keywords = "Disturbance observer, Flexible spacecraft, Input magnitude and rate constraints, LMI technology, State feedback control",

author = "Zhijie Liu and Jinkun Liu and Lijun Wang",

note = "Publisher Copyright: {\textcopyright} 2017 Elsevier Masson SAS",

year = "2018",

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AU - Liu, Jinkun

AU - Wang, Lijun

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N2 - In this paper, we investigate the problem of attitude control design for flexible spacecraft with external disturbance, input magnitude and rate constraints. First, a disturbance observer is designed to estimate and compensate for the disturbances including the external disturbance and vibration from the flexible appendages. Then, based on the disturbance observer, a sample state feedback control scheme is proposed for flexible spacecraft subject to input magnitude and rate constrains, using the linear matrix inequality (LMI) and Lyapunov direct method. Finally, the results are illustrated using numerical simulations for control performance verification.

AB - In this paper, we investigate the problem of attitude control design for flexible spacecraft with external disturbance, input magnitude and rate constraints. First, a disturbance observer is designed to estimate and compensate for the disturbances including the external disturbance and vibration from the flexible appendages. Then, based on the disturbance observer, a sample state feedback control scheme is proposed for flexible spacecraft subject to input magnitude and rate constrains, using the linear matrix inequality (LMI) and Lyapunov direct method. Finally, the results are illustrated using numerical simulations for control performance verification.

KW - Disturbance observer

KW - Flexible spacecraft

KW - Input magnitude and rate constraints

KW - LMI technology

KW - State feedback control

UR - https://www.scopus.com/pages/publications/85037156909

U2 - 10.1016/j.ast.2017.11.036

DO - 10.1016/j.ast.2017.11.036

M3 - 文章

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SN - 1270-9638

VL - 72

SP - 486

EP - 492

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

ER -

Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints

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Keywords

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