Fractional-Order Sliding Mode Guidance Law for Intercepting Hypersonic Vehicles
This paper addresses the problem of a low-speed missile intercepting a hypersonic vehicle in the longitudinal plane. Firstly, based on the concept of the zero of the angular rate of the line-of-sight (LOS) angle, the guidance system is established by defining the LOS angular rate as the state variab...
| Main Authors: | , , , , |
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| Formato: | Artigo |
| Idioma: | English |
| Publicado: |
MDPI AG
2022-01-01
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| Series: | Aerospace |
| Subjects: | |
| Acceso en liña: | https://www.mdpi.com/2226-4310/9/2/53 |