A Control Method for Thermal Structural Tests of Hypersonic Missile Aerodynamic Heating

This paper presents an intelligent proportional-derivative adaptive global nonsingular fast-terminal sliding-mode control (IPDAGNFTSMC) for tracking temperature trajectories of a hypersonic missile in thermal structural tests. Firstly, the numerical analyses on a hypersonic missile’s aerodynamic hea...

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發表在:	Mathematics
Main Authors:	Chao Lu, Guangming Zhang, Xiaodong Lv
格式:	Article
語言:	英语
出版:	MDPI AG 2025-01-01
主題:	hypersonic missile thermal structural test sliding mode control
在線閱讀:	https://www.mdpi.com/2227-7390/13/3/380