### 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 language | English |
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Pages (from-to) | 1098-1103 |

Number of pages | 6 |

Journal | Proceedings of the American Control Conference |

Volume | 2 |

Publication status | Published - 2003 Nov 7 |

Event | 2003 American Control Conference - Denver, CO, United States Duration: 2003 Jun 4 → 2003 Jun 6 |

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### All Science Journal Classification (ASJC) codes

- Electrical and Electronic Engineering

### Cite this

*Proceedings of the American Control Conference*,

*2*, 1098-1103.

}

*Proceedings of the American Control Conference*, vol. 2, pp. 1098-1103.

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

Research output: Contribution to journal › Conference article

TY - JOUR

T1 - Satellite Large Angle Tracking Control Design

T2 - Thruster Control Approach

AU - Show, Long Life

AU - Juang, Jyh-Chin

PY - 2003/11/7

Y1 - 2003/11/7

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.

UR - http://www.scopus.com/inward/record.url?scp=0142231447&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0142231447&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:0142231447

VL - 2

SP - 1098

EP - 1103

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

SN - 0743-1619

ER -