| Autor: |
Siyu Qiao, Zhonghua Wu, Bojun Liu, Mingshan Hou, Wencong Wang |
| Rok vydání: |
2021 |
| Předmět: |
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| Zdroj: |
2021 40th Chinese Control Conference (CCC). |
| DOI: |
10.23919/ccc52363.2021.9549297 |
| Popis: |
A novel predefined-time attitude tracking control method is proposed for a rigid spacecraft. It is required that the attitude tracking error can converge to zero or a small neighborhood of zero in a finite time, whose upper bound is exactly a positive constant parameter that can be set arbitrarily by users. Two definitions about global predefined-time stability and global predefined-time boundedness are given. Time-varying tuning functions are introduced into the backstepping-based attitude control designs. Lyapunov approach proves the system stability and simulation results verify the effectiveness of the controllers. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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