Integrity fault tolerant attitude controller of satellite with disturbance attenuation

Jing Yang; Xiao Ping Shi

doi:10.3969/j.issn.1001-506X.2013.01.21

Integrity fault tolerant attitude controller of satellite with disturbance attenuation

Jing Yang^*
, Xiao Ping Shi

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology

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

5 Scopus citations

Abstract

An integrity fault tolerant control problem of uncertain linear system is studied. Based on the Riccati equation and linear matrix inequality, an integrity fault tolerant attitude controller with disturbance attenuation is designed for the actuator failure of the satellite by using four reaction wheels. Furthermore, the conclusion that the designed controller can be applied to more kinds of actuator failure forms can be drawn. The simulation on the satellite attitude system demonstrates the correctness and effectiveness of the proposed method.

Original language	English
Pages (from-to)	126-131
Number of pages	6
Journal	Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
Volume	35
Issue number	1
DOIs	https://doi.org/10.3969/j.issn.1001-506X.2013.01.21
State	Published - Jan 2013
Externally published	Yes

Keywords

Attitude controller of satellite
Disturbance attenuation
Fault tolerant control
Integrity

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Cite this

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abstract = "An integrity fault tolerant control problem of uncertain linear system is studied. Based on the Riccati equation and linear matrix inequality, an integrity fault tolerant attitude controller with disturbance attenuation is designed for the actuator failure of the satellite by using four reaction wheels. Furthermore, the conclusion that the designed controller can be applied to more kinds of actuator failure forms can be drawn. The simulation on the satellite attitude system demonstrates the correctness and effectiveness of the proposed method.",

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AB - An integrity fault tolerant control problem of uncertain linear system is studied. Based on the Riccati equation and linear matrix inequality, an integrity fault tolerant attitude controller with disturbance attenuation is designed for the actuator failure of the satellite by using four reaction wheels. Furthermore, the conclusion that the designed controller can be applied to more kinds of actuator failure forms can be drawn. The simulation on the satellite attitude system demonstrates the correctness and effectiveness of the proposed method.

KW - Attitude controller of satellite

KW - Disturbance attenuation

KW - Fault tolerant control

KW - Integrity

UR - https://www.scopus.com/pages/publications/84874500835

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JF - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics

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ER -

Integrity fault tolerant attitude controller of satellite with disturbance attenuation

Abstract

Keywords

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