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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...

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Detalhes bibliográficos
Main Authors: Jianguo Guo, Xinming Wang, Jun Zhou
Formato: Artigo
Idioma:Inglês
Publicado em: SAGE Publishing 2018-04-01
Colecção:Advances in Mechanical Engineering
Acesso em linha:https://doi.org/10.1177/1687814018769449
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