Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

Yon-Ping Chen; Shih Che Lo

doi:10.1109/7.259536

Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

Yon-Ping Chen
, Shih Che Lo

國立陽明交通大學

研究成果: Article › 同行評審

193 引文斯高帕斯（Scopus）

摘要

This paper presents a robust sliding-mode control law to deal with the spacecraft attitude tracking problems. Two important natural properties related to the spacecraft model of motion are shown and then by using these properties and the second method of Lyapunov theory, the system stability in the sliding mode can be easily achieved. The success of the sliding-mode controller and the robustness to uncertainties are illustrated by an example of multiaxial attitude tracking maneuvers.

原文	English
頁（從 - 到）	1328-1333
頁數	6
期刊	IEEE Transactions on Aerospace and Electronic Systems
卷	29
發行號	4
DOIs	https://doi.org/10.1109/7.259536
出版狀態	Published - 10月 1993

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10.1109/7.259536

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abstract = "This paper presents a robust sliding-mode control law to deal with the spacecraft attitude tracking problems. Two important natural properties related to the spacecraft model of motion are shown and then by using these properties and the second method of Lyapunov theory, the system stability in the sliding mode can be easily achieved. The success of the sliding-mode controller and the robustness to uncertainties are illustrated by an example of multiaxial attitude tracking maneuvers.",

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Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

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