标题: | Fixed-time attitude tracking control for rigid spacecraft |
时间: | 2021-04-08 16:27:26 |
DOI: | 10.1016/j.automatica.2019.108792 |
大小: | 1315 kb |
页数: | 10 PAGES |
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目录:
- Preassigned finite-time attitude control for spacecraft based on time-varying barrier Lyapunov functions
- 1 Introduction
- 2 Spacecraft modeling and problem formulation
- 3 Attitude tracking controller design
- 4 Simulation results
- 5 Conclusion
- Declaration of competing interest
- Acknowledgement
- References
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