Controlling chaotic attitude motion of spacecraft by the input-output linearization

L. Q. Chen; Y. Z. Liu

doi:10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y

Controlling chaotic attitude motion of spacecraft by the input-output linearization

L. Q. Chen^*
, Y. Z. Liu

^*Corresponding author for this work

Shanghai University
Shanghai Jiao Tong University

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

6 Scopus citations

Abstract

In this paper, the control of chaotic osculations is investigated. A nonlinear control methodology termed input-output linearization is utilized. Chaotic attitude motion of a spacecraft moving on an elliptic orbit in the gravitational field with both air drag and internal damping is treated as an example.

Original language	English
Pages (from-to)	701-704
Number of pages	4
Journal	ZAMM Zeitschrift fur Angewandte Mathematik und Mechanik
Volume	80
Issue number	10
DOIs	https://doi.org/10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y
State	Published - 2000
Externally published	Yes

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10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y

Cite this

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title = "Controlling chaotic attitude motion of spacecraft by the input-output linearization",

abstract = "In this paper, the control of chaotic osculations is investigated. A nonlinear control methodology termed input-output linearization is utilized. Chaotic attitude motion of a spacecraft moving on an elliptic orbit in the gravitational field with both air drag and internal damping is treated as an example.",

author = "Chen, \{L. Q.\} and Liu, \{Y. Z.\}",

year = "2000",

doi = "10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y",

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AU - Chen, L. Q.

AU - Liu, Y. Z.

PY - 2000

Y1 - 2000

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AB - In this paper, the control of chaotic osculations is investigated. A nonlinear control methodology termed input-output linearization is utilized. Chaotic attitude motion of a spacecraft moving on an elliptic orbit in the gravitational field with both air drag and internal damping is treated as an example.

UR - https://www.scopus.com/pages/publications/23044524053

U2 - 10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y

DO - 10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y

M3 - 文章

AN - SCOPUS:23044524053

SN - 0044-2267

VL - 80

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JO - ZAMM Zeitschrift fur Angewandte Mathematik und Mechanik

JF - ZAMM Zeitschrift fur Angewandte Mathematik und Mechanik

IS - 10

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Controlling chaotic attitude motion of spacecraft by the input-output linearization

Abstract

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