Satellite Large Angle Tracking Control Design: Thruster Control Approach

Long Life Show, Jyh Ching Juang

研究成果: Conference article

10 引文 (Scopus)

摘要

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.

原文English
頁(從 - 到)1098-1103
頁數6
期刊Proceedings of the American Control Conference
2
出版狀態Published - 2003 十一月 7
事件2003 American Control Conference - Denver, CO, United States
持續時間: 2003 六月 42003 六月 6

指紋

Satellites
Robust control
Trajectories
Attitude control
Stabilization

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

引用此文

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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.",
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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.

AB - 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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