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Sliding Mode Control Applied to a Mini-Aircraft Pitch Position Model

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Détails bibliographiques
Auteur principal:	Ricardo Carreño Aguilera
Format:	Artículo científico
Langue:	en
Publié:	Instituto Politécnico Nacional 2014
Sujets:	Computación mini Sliding modes aircraft models integral and proportional control
Accès en ligne:	Acceder al recurso
Tags:	Ajouter un tag Pas de tags, Soyez le premier à ajouter un tag!

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