Sliding Mode Backstepping Control for the Ascent Phase of Near-Space Hypersonic Vehicle Based on a Novel Triple Power Reaching Law

This paper presents a novel sliding mode backstepping control scheme for the ascent phase of a near-space hypersonic vehicle (NSHV) base on a triple power reaching law (TPRL). A new model transformation is proposed for NSHV with uncertain parameters subject to uncertainties during ascent phase. To s...

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Bibliographic Details
Main Authors: Shutong Huang, Ju Jiang, Ouxun Li
Format: Article
Language:English
Published: MDPI AG 2022-11-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/12/755