Research on the Attitude Control Law of Hypersonic Flight Vehicle
Hypersonic flight vehicle has strong-nonlinearity, quick time-variability, strong-coupling features. In order to realize its flight effective control, the airflow attitude angle needs to be controlled precisely. Based on the accurate tracking of the airflow attitude angle command, the predetermined...
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| Автори: | , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
AIDIC Servizi S.r.l.
2015-12-01
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| Серія: | Chemical Engineering Transactions |
| Онлайн доступ: | https://www.cetjournal.it/index.php/cet/article/view/4196 |
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