Improved Adaptive Integral-Sliding-Mode Fault-Tolerant Control for Hypersonic Vehicle With Actuator Fault
In this paper, the problem of attitude control for hypersonic vehicle in the present of actuator fault and unknown uncertainties including modeling uncertainties, aerodynamic parameters uncertainties is investigated based on integral sliding mode technique. A fault-tolerant control (FTC) law is prop...
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| Главные авторы: | , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
IEEE
2021-01-01
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| Серии: | IEEE Access |
| Предметы: | |
| Online-ссылка: | https://ieeexplore.ieee.org/document/9381209/ |
| Метки: |
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