Adaptive finite-time attitude control for spacecraft with input quantization and measurement uncertainties
The issue of adaptive finite-time attitude control is explored for rigid spacecraft with input quantization and measurement uncertainties, in which a hysteretic quantizer is introduced. The measurement uncertainties and external disturbances are compensated via adaptive control technique. By combini...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2019-05-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/1687814019853108 |