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An improved predictor–corrector entry guidance method for hypersonic flight vehicle
This article improves an enhanced predictor–corrector entry guidance method for hypersonic flight vehicle. To compensate for the shortcoming that the enhanced predictor–corrector guidance method sacrifices guidance precision to meet path constraints, this article develops an improved predictor–corre...
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| Main Authors: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
SAGE Publishing
2017-10-01
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| Colecção: | Advances in Mechanical Engineering |
| Acesso em linha: | https://doi.org/10.1177/1687814017726291 |
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