Cooperative Smooth Nonsingular Terminal Sliding Mode Guidance with Tracking Differentiator for Active Aircraft Defense

Aimed at the poor performance of guidance algorithms designed based on a linearized model in active defense under large leading angle deviation, both-way and one-way cooperative sliding mode guidance algorithms based on the smooth nonsingular terminal sliding mode for the defense missile are propose...

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Auteurs principaux:	Quancheng Li, Yonghua Fan, Tian Yan, Xuechao Liang, Jie Yan
Format:	Artigo
Langue:	Inglês
Publié:	MDPI AG 2022-04-01
Collection:	Aerospace
Sujets:	smooth nonsingular terminal sliding mode finite-time convergence cooperative guidance tracking differentiator active defense
Accès en ligne:	https://www.mdpi.com/2226-4310/9/4/221
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