### 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 |

卷 | 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 4 → 2003 六月 6 |

### 指紋

### All Science Journal Classification (ASJC) codes

- Electrical and Electronic Engineering

### 引用此文

*Proceedings of the American Control Conference*,

*2*, 1098-1103.

}

*Proceedings of the American Control Conference*, 卷 2, 頁 1098-1103.

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

研究成果: Conference article

TY - JOUR

T1 - Satellite Large Angle Tracking Control Design

T2 - Thruster Control Approach

AU - Show, Long Life

AU - Juang, Jyh Ching

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 -