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 |
|---|---|
| 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 |
All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering