Guaranteed performance control of nonlinear dynamic systems arising from large flexible space structures

Y. D. SONG

doi:10.1109/ACC.1994.751742

Guaranteed performance control of nonlinear dynamic systems arising from large flexible space structures

Y. D. SONG^*

^*Corresponding author for this work

Research output: Book Chapters | Papers in Conference Proceedings › Conference paper (refereed) › Research › peer-review

Abstract

This paper considers the control problem of nonlinear uncertain systems arising from flexible aerospace structures. We begin by addressing the tracking problem of a class of nonlinear dynamic systems with modeling uncertainties and external disturbances. New control algorithms against modeling uncertainties are proposed. It is shown that these algorithms not only guarantee system stability, but also achieve certain bounded performance index, and they are readily applicable in vibration suppression of large flexible space structures. Numerical verification of the proposed strategy is demonstrated via the lumped mass model of a hypersonic aerospace flight vehicle structure.

Original language	English
Title of host publication	Proceedings of the 1994 American Control Conference
Publisher	IEEE
Pages	278-282
Number of pages	5
ISBN (Print)	0780317831
DOIs	https://doi.org/10.1109/ACC.1994.751742
Publication status	Published - 1994
Externally published	Yes
Event	1994 American Control Conference - Baltimore, United States Duration: 29 Jun 1994 → 1 Jul 1994

Publication series

Name	Proceedings of the American Control Conference
Publisher	IEEE
ISSN (Print)	0743-1619

Conference

Conference	1994 American Control Conference
Country/Territory	United States
City	Baltimore
Period	29/06/94 → 1/07/94

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10.1109/ACC.1994.751742

Cite this

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title = "Guaranteed performance control of nonlinear dynamic systems arising from large flexible space structures",

abstract = "This paper considers the control problem of nonlinear uncertain systems arising from flexible aerospace structures. We begin by addressing the tracking problem of a class of nonlinear dynamic systems with modeling uncertainties and external disturbances. New control algorithms against modeling uncertainties are proposed. It is shown that these algorithms not only guarantee system stability, but also achieve certain bounded performance index, and they are readily applicable in vibration suppression of large flexible space structures. Numerical verification of the proposed strategy is demonstrated via the lumped mass model of a hypersonic aerospace flight vehicle structure.",

author = "SONG, \{Y. D.\}",

year = "1994",

doi = "10.1109/ACC.1994.751742",

language = "English",

isbn = "0780317831",

series = "Proceedings of the American Control Conference",

publisher = "IEEE",

pages = "278--282",

booktitle = "Proceedings of the 1994 American Control Conference",

note = "1994 American Control Conference ; Conference date: 29-06-1994 Through 01-07-1994",

}

Guaranteed performance control of nonlinear dynamic systems arising from large flexible space structures. / SONG, Y. D.
Proceedings of the 1994 American Control Conference. IEEE, 1994. p. 278-282 (Proceedings of the American Control Conference).

Research output: Book Chapters | Papers in Conference Proceedings › Conference paper (refereed) › Research › peer-review

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PY - 1994

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N2 - This paper considers the control problem of nonlinear uncertain systems arising from flexible aerospace structures. We begin by addressing the tracking problem of a class of nonlinear dynamic systems with modeling uncertainties and external disturbances. New control algorithms against modeling uncertainties are proposed. It is shown that these algorithms not only guarantee system stability, but also achieve certain bounded performance index, and they are readily applicable in vibration suppression of large flexible space structures. Numerical verification of the proposed strategy is demonstrated via the lumped mass model of a hypersonic aerospace flight vehicle structure.

AB - This paper considers the control problem of nonlinear uncertain systems arising from flexible aerospace structures. We begin by addressing the tracking problem of a class of nonlinear dynamic systems with modeling uncertainties and external disturbances. New control algorithms against modeling uncertainties are proposed. It is shown that these algorithms not only guarantee system stability, but also achieve certain bounded performance index, and they are readily applicable in vibration suppression of large flexible space structures. Numerical verification of the proposed strategy is demonstrated via the lumped mass model of a hypersonic aerospace flight vehicle structure.

UR - https://www.scopus.com/pages/publications/0028584927

U2 - 10.1109/ACC.1994.751742

DO - 10.1109/ACC.1994.751742

M3 - Conference paper (refereed)

AN - SCOPUS:0028584927

SN - 0780317831

T3 - Proceedings of the American Control Conference

SP - 278

EP - 282

BT - Proceedings of the 1994 American Control Conference

PB - IEEE

T2 - 1994 American Control Conference

Y2 - 29 June 1994 through 1 July 1994

ER -

Guaranteed performance control of nonlinear dynamic systems arising from large flexible space structures

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