Spacecraft attitude tracking control

Shih Che Lo; Yon-Ping Chen

doi:10.1109/ACC.1995.532094

Spacecraft attitude tracking control

Shih Che Lo^*, Yon-Ping Chen

^*Corresponding author for this work

Department of Electrical and Computer Engineering

Research output: Contribution to journal › Conference article › peer-review

Abstract

In this paper, we investigate the properties of some special classes of matrices and, from these properties, we find an orthogonal transformation with which the attitude tracking problem can be treated as a regulation problem. In addition, these properties are also used to design the smoothing model-reference sliding-mode control (SMRSMC) law of the spacecraft attitude tracking maneuvers. First, a set of linear sliding manifolds are chosen in the sliding-mode controller (SMC) to achieve the robust and global attitude tracking maneuvers of spacecrafts. Next, the smoothing reference model is given and discussed. Finally, a numerical example is included to demonstrate the success of the developed SMRSMC.

Original language	English
Article number	532094
Pages (from-to)	3136-3140
Number of pages	5
Journal	Proceedings of the American Control Conference
Volume	5
DOIs	https://doi.org/10.1109/ACC.1995.532094
State	Published - 21 Jun 1995
Event	Proceedings of the 1995 American Control Conference. Part 1 (of 6) - Seattle, WA, USA Duration: 21 Jun 1995 → 23 Jun 1995

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title = "Spacecraft attitude tracking control",

abstract = "In this paper, we investigate the properties of some special classes of matrices and, from these properties, we find an orthogonal transformation with which the attitude tracking problem can be treated as a regulation problem. In addition, these properties are also used to design the smoothing model-reference sliding-mode control (SMRSMC) law of the spacecraft attitude tracking maneuvers. First, a set of linear sliding manifolds are chosen in the sliding-mode controller (SMC) to achieve the robust and global attitude tracking maneuvers of spacecrafts. Next, the smoothing reference model is given and discussed. Finally, a numerical example is included to demonstrate the success of the developed SMRSMC.",

author = "Lo, {Shih Che} and Yon-Ping Chen",

year = "1995",

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doi = "10.1109/ACC.1995.532094",

language = "English",

volume = "5",

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journal = "Proceedings of the American Control Conference",

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note = "Proceedings of the 1995 American Control Conference. Part 1 (of 6) ; Conference date: 21-06-1995 Through 23-06-1995",

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AU - Lo, Shih Che

AU - Chen, Yon-Ping

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N2 - In this paper, we investigate the properties of some special classes of matrices and, from these properties, we find an orthogonal transformation with which the attitude tracking problem can be treated as a regulation problem. In addition, these properties are also used to design the smoothing model-reference sliding-mode control (SMRSMC) law of the spacecraft attitude tracking maneuvers. First, a set of linear sliding manifolds are chosen in the sliding-mode controller (SMC) to achieve the robust and global attitude tracking maneuvers of spacecrafts. Next, the smoothing reference model is given and discussed. Finally, a numerical example is included to demonstrate the success of the developed SMRSMC.

AB - In this paper, we investigate the properties of some special classes of matrices and, from these properties, we find an orthogonal transformation with which the attitude tracking problem can be treated as a regulation problem. In addition, these properties are also used to design the smoothing model-reference sliding-mode control (SMRSMC) law of the spacecraft attitude tracking maneuvers. First, a set of linear sliding manifolds are chosen in the sliding-mode controller (SMC) to achieve the robust and global attitude tracking maneuvers of spacecrafts. Next, the smoothing reference model is given and discussed. Finally, a numerical example is included to demonstrate the success of the developed SMRSMC.

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U2 - 10.1109/ACC.1995.532094

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M3 - Conference article

AN - SCOPUS:0029191219

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EP - 3140

JO - Proceedings of the American Control Conference

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M1 - 532094

T2 - Proceedings of the 1995 American Control Conference. Part 1 (of 6)

Y2 - 21 June 1995 through 23 June 1995

ER -

Spacecraft attitude tracking control

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