Abstract
This paper presents a new control method for satellite attitude control systems with input constraints. By augmenting a bounded hyperbolic tangent function into the control variables, the attitude control system is transformed to a higher-order configuration, thereby solving the input constraint issue. The obtained controller enables finite-time stability for the attitude control system. It demonstrates that the convergence time of the state trajectory is inversely proportional with the input constraints. The efficacy of the proposed approach is validated through simulation examples.
| Original language | English |
|---|---|
| Pages | 256-261 |
| Number of pages | 6 |
| DOIs | |
| State | Published - 2025 |
| Event | 15th International Workshop on Computer Science and Engineering, WCSE 2025 - Jeju Island, Korea, Republic of Duration: 28 Jun 2025 → 30 Jun 2025 |
Conference
| Conference | 15th International Workshop on Computer Science and Engineering, WCSE 2025 |
|---|---|
| Country/Territory | Korea, Republic of |
| City | Jeju Island |
| Period | 28/06/25 → 30/06/25 |
Keywords
- Attitude control
- Finite-time stability
- Input constraints
- Rigid satellite
Fingerprint
Dive into the research topics of 'A New Attitude Control Method Reveals Relationship Between Stabilization Time and Input Constraints'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver