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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| Hauptverfasser: | , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
MDPI AG
2025-01-01
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| Schriftenreihe: | Mathematics |
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| Online-Zugang: | https://www.mdpi.com/2227-7390/13/3/380 |
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