Exo-atmospheric guidance of an accelerating interceptor missile

DOI10.1016/J.JFRANKLIN.2011.06.024zbMath1254.93056OpenAlexW2080499490MaRDI QIDQ1933454

Tal Shima, Oded M. Golan

Publication date: 24 January 2013

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2011.06.024

zbMATH Keywords

sliding mode controlnavigation guidance law

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Variable structure systems (93B12) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (3)

A Differential Game Based Guidance Law for an Accelerating Exoatmospheric Missile ⋮ Integrated interceptor guidance and control with prescribed performance ⋮ Scale-based cluster formation for multi-agent systems with mismatched disturbances

Cites Work

• Sliding modes in control and optimization. Transl. from the Russian
• Smooth second-order sliding modes: missile guidance application
• Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics
• Higher-order sliding modes, differentiation and output-feedback control
• Unnamed Item

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