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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Detalhes bibliográficos

Principais autores:	Fazhan Tao, Jingtian Shi, Jie Zhang, Zhumu Fu, Song Gao
Formato:	Artigo
Idioma:	Inglês
Publicado em:	Instituto de Aeronáutica e Espaço (IAE) 2024-02-01
Colecção:	Journal of Aerospace Technology and Management
Assuntos:	Terminal guidance Targets Angle of attack Missile control
Acesso em linha:	https://jatm.com.br/jatm/article/view/1324
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