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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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Principais autores: Quancheng Li, Yonghua Fan, Tian Yan, Xuechao Liang, Jie Yan
פורמט: Artigo
שפה:Inglês
יצא לאור: MDPI AG 2022-04-01
סדרה:Aerospace
נושאים:
smooth nonsingular terminal sliding mode
finite-time convergence
cooperative guidance
tracking differentiator
active defense
גישה מקוונת:https://www.mdpi.com/2226-4310/9/4/221
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