Publication

Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking

Zhou, N., Kawano, Y. & Cao, M., 2019, Proceedings of the IFAC LSS 2019. Elsevier, p. 67-72 6 p. (IFAC-PapersOnLine; vol. 52, no. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

APA

Zhou, N., Kawano, Y., & Cao, M. (2019). Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking. In Proceedings of the IFAC LSS 2019 (pp. 67-72). (IFAC-PapersOnLine; Vol. 52, No. 3). Elsevier. https://doi.org/10.1016/j.ifacol.2019.06.012

Author

Zhou, Ning ; Kawano, Yu ; Cao, Ming. / Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking. Proceedings of the IFAC LSS 2019. Elsevier, 2019. pp. 67-72 (IFAC-PapersOnLine; 3).

Harvard

Zhou, N, Kawano, Y & Cao, M 2019, Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking. in Proceedings of the IFAC LSS 2019. IFAC-PapersOnLine, no. 3, vol. 52, Elsevier, pp. 67-72, 15th IFAC Large Scale Complex Systems symposium (IFAC LSS2019), Delft, Netherlands, 26/05/2019. https://doi.org/10.1016/j.ifacol.2019.06.012

Standard

Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking. / Zhou, Ning; Kawano, Yu; Cao, Ming.

Proceedings of the IFAC LSS 2019. Elsevier, 2019. p. 67-72 (IFAC-PapersOnLine; Vol. 52, No. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

Vancouver

Zhou N, Kawano Y, Cao M. Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking. In Proceedings of the IFAC LSS 2019. Elsevier. 2019. p. 67-72. (IFAC-PapersOnLine; 3). https://doi.org/10.1016/j.ifacol.2019.06.012


BibTeX

@inproceedings{a5ede2d2897745a586c6eb778ea9504b,
title = "Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking",
abstract = "An intelligent failure-tolerant approach is proposed for attitude tracking control of a rigid spacecraft. To deal with the integrated troublesome of model uncertainties, external disturbances and subsystem faults and failures, ideas from artificial intelligence are used for integrating and parameterizing the system model. Furthermore, the adaptive control technique is employed to estimate the unique design parameter extracting from the reconstructed model under bounded disturbances. With the help of Lyapunov theory, we show that the proposed method guarantees the failure-tolerance capability of the closed-loop systems. Finally, the feasibility of the proposed method is illustrated through numerical examples.",
author = "Ning Zhou and Yu Kawano and Ming Cao",
year = "2019",
doi = "10.1016/j.ifacol.2019.06.012",
language = "English",
series = "IFAC-PapersOnLine",
publisher = "Elsevier",
number = "3",
pages = "67--72",
booktitle = "Proceedings of the IFAC LSS 2019",

}

RIS

TY - GEN

T1 - Adaptive Failure-Tolerant Control for Spacecraft Attitude Tracking

AU - Zhou, Ning

AU - Kawano, Yu

AU - Cao, Ming

PY - 2019

Y1 - 2019

N2 - An intelligent failure-tolerant approach is proposed for attitude tracking control of a rigid spacecraft. To deal with the integrated troublesome of model uncertainties, external disturbances and subsystem faults and failures, ideas from artificial intelligence are used for integrating and parameterizing the system model. Furthermore, the adaptive control technique is employed to estimate the unique design parameter extracting from the reconstructed model under bounded disturbances. With the help of Lyapunov theory, we show that the proposed method guarantees the failure-tolerance capability of the closed-loop systems. Finally, the feasibility of the proposed method is illustrated through numerical examples.

AB - An intelligent failure-tolerant approach is proposed for attitude tracking control of a rigid spacecraft. To deal with the integrated troublesome of model uncertainties, external disturbances and subsystem faults and failures, ideas from artificial intelligence are used for integrating and parameterizing the system model. Furthermore, the adaptive control technique is employed to estimate the unique design parameter extracting from the reconstructed model under bounded disturbances. With the help of Lyapunov theory, we show that the proposed method guarantees the failure-tolerance capability of the closed-loop systems. Finally, the feasibility of the proposed method is illustrated through numerical examples.

U2 - 10.1016/j.ifacol.2019.06.012

DO - 10.1016/j.ifacol.2019.06.012

M3 - Conference contribution

T3 - IFAC-PapersOnLine

SP - 67

EP - 72

BT - Proceedings of the IFAC LSS 2019

PB - Elsevier

ER -

ID: 109698576