Attitude Stabilization Control for Underactuated Spacecraft: A Predefined-Time Method
The attitude controller design for the underactuated rigid spacecraft is addressed by considering that there are only 2 reaction wheels in the spacecraft. Most of the existing attitude control methods for underactuated spacecraft suffer from long system state convergence times and large overshoots....
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
American Association for the Advancement of Science (AAAS)
2025-01-01
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| Series: | Space: Science & Technology |
| Online Access: | https://spj.science.org/doi/10.34133/space.0272 |
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