Satellite Large Angle Tracking Control Design: Thruster Control Approach

Long Life Show, Jyh-Chin Juang

Research output: Contribution to journalConference article

10 Citations (Scopus)

Abstract

The paper presents a nonlinear robust control design method for satellite with asymptotic tracking of a desired attitude trajectory based on thruster. The error dynamics with respect to a given reference trajectory is derived and the design procedure is formulated as a stabilization problem. The solution of the nonlinear robust control problem is known to related to the existence of solution to a Hamilton-Jacobi inequality. A candidate solution to the Hamilton-Jacobi inequality is obtained for the attitude control problem. The method is applied to the ROCSAT-3 attitude tracking control problem to verify its effectiveness. large angle tracking control, Hamilton-Jacobi inequality, thruster control.

Original languageEnglish
Pages (from-to)1098-1103
Number of pages6
JournalProceedings of the American Control Conference
Volume2
Publication statusPublished - 2003 Nov 7
Event2003 American Control Conference - Denver, CO, United States
Duration: 2003 Jun 42003 Jun 6

Fingerprint

Satellites
Robust control
Trajectories
Attitude control
Stabilization

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

Cite this

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Satellite Large Angle Tracking Control Design : Thruster Control Approach. / Show, Long Life; Juang, Jyh-Chin.

In: Proceedings of the American Control Conference, Vol. 2, 07.11.2003, p. 1098-1103.

Research output: Contribution to journalConference article

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AU - Juang, Jyh-Chin

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N2 - The paper presents a nonlinear robust control design method for satellite with asymptotic tracking of a desired attitude trajectory based on thruster. The error dynamics with respect to a given reference trajectory is derived and the design procedure is formulated as a stabilization problem. The solution of the nonlinear robust control problem is known to related to the existence of solution to a Hamilton-Jacobi inequality. A candidate solution to the Hamilton-Jacobi inequality is obtained for the attitude control problem. The method is applied to the ROCSAT-3 attitude tracking control problem to verify its effectiveness. large angle tracking control, Hamilton-Jacobi inequality, thruster control.

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