Integrated guidance and control for dual-control missiles based on small-gain theorem

DOI10.1016/j.automatica.2012.06.084zbMath1271.93053OpenAlexW2074578621MaRDI QIDQ361059

Han Yan, Hai-Bo Ji

Publication date: 28 August 2013

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S0005109812003548

zbMATH Keywords

robustnessinput-to-state stabilityintegrated guidance and controlsmall-gain theorem

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) Adaptive or robust stabilization (93D21)

Related Items (3)

Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception ⋮ Stabilizing region of \(PD^\mu\) controller for fractional order system with general interval uncertainties and an interval delay ⋮ Neural learning control of missile interception against dynamics uncertainty and target evasive maneuver

Cites Work

• Small-gain theorem for ISS systems and applications
• Smooth second-order sliding modes: missile guidance application
• Smooth stabilization implies coprime factorization

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