Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory

DOI10.1080/00207179.2012.675519zbMath1304.49080OpenAlexW2070389089MaRDI QIDQ5745604

Xiao Sun, Yuanqing Xia

Publication date: 30 January 2014

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

Full work available at URL: https://doi.org/10.1080/00207179.2012.675519

zbMATH Keywords

optimal control theoryoptimal guidance law

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control problems involving ordinary differential equations (34H05)

Related Items (3)

Cooperative guidance laws for interception of active maneuvering target under information symmetric and asymmetric conditions ⋮ Cooperative guidance for simultaneous attack: a fully distributed, adaptive, and optimal approach ⋮ Finite-time intercept-angle guidance

Cites Work

• Optimal Guidance with Reduced Sensitivity to Time-to-Go Estimation Errors
• Optimal guidance law in the plane
• Minimum Energy Guidance for Aerodynamically Controlled Missiles

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