Robust Finite-Time Control for Guidance Law with Uncertainties in Missile Dynamics
In this paper, the robust !nite-time control for impact angle guidance of missile dynamic system with uncertainties is investigated by combining linear extended state observer (LESO) and adaptive non-singular fast terminal sliding mode method. Specially for dealing with existing uncertainties inclu...
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| Autors principals: | , , , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Instituto de Aeronáutica e Espaço (IAE)
2024-02-01
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| Col·lecció: | Journal of Aerospace Technology and Management |
| Matèries: | |
| Accés en línia: | https://jatm.com.br/jatm/article/view/1324 |
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