Integrated guidance and control of hypersonic flight vehicle with coordinated mission requirement and input constraint

DOI10.1002/rnc.6607OpenAlexW4319836057MaRDI QIDQ6190216

Fuchun Sun, Tian Yan, Unnamed Author, Bin Xu

Publication date: 6 February 2024

Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/rnc.6607

zbMATH Keywords

neural networkhypersonic flight vehicleinput constraintintegrated guidance and controlKarush-Kuhn-Tucker condition

Mathematics Subject Classification ID

Control/observation systems governed by partial differential equations (93C20) Application models in control theory (93C95) Adaptive control/observation systems (93C40)

Cites Work

• Continuous finite-time control for robotic manipulators with terminal sliding mode
• Three-dimensional optimal pursuit and evasion with bounded controls
• Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation

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