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Attitude control precision analysis for hypersonic vehicles based on covariance analysis describing equation technique
This article investigates a control precision analysis based on covariance analysis describing equation technique for the generic hypersonic vehicle attitude tracking system. For a nominal generic hypersonic vehicle attitude system, a global sliding mode control strategy is pointed out first and the...
Kaydedildi:
| Asıl Yazarlar: | , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
SAGE Publishing
2018-04-01
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| Seri Bilgileri: | Advances in Mechanical Engineering |
| Online Erişim: | https://doi.org/10.1177/1687814018769449 |
| Etiketler: |
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