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

National Yang Ming Chiao Tung University

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

189 Scopus citations

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.

Original language	English
Pages (from-to)	1328-1333
Number of pages	6
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	29
Issue number	4
DOIs	https://doi.org/10.1109/7.259536
State	Published - Oct 1993

Access to Document

10.1109/7.259536

Cite this

@article{f1ef840310de4fa68baee8ba636ca97c,

title = "Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers",

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.",

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

year = "1993",

month = oct,

doi = "10.1109/7.259536",

language = "English",

volume = "29",

pages = "1328--1333",

journal = "IEEE Transactions on Aerospace and Electronic Systems",

issn = "0018-9251",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

number = "4",

}

TY - JOUR

T1 - Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

AU - Chen, Yon-Ping

AU - Lo, Shih Che

PY - 1993/10

Y1 - 1993/10

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=0027683644&partnerID=8YFLogxK

U2 - 10.1109/7.259536

DO - 10.1109/7.259536

M3 - Article

AN - SCOPUS:0027683644

SN - 0018-9251

VL - 29

SP - 1328

EP - 1333

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 4

ER -

Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

Abstract

Access to Document

Other files and links

Fingerprint

Cite this