Design of an adaptive missile autopilot considering the boost phase using the SDRE method and neural networks

DOI10.1016/j.jfranklin.2016.12.004zbMath1404.93021OpenAlexW2560829564MaRDI QIDQ1634447

Youdan Kim, Yongwoo Lee, Byung-Eul Jun, Gwanyoung Moon, Jae-Ho Lee

Publication date: 18 December 2018

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2016.12.004

zbMATH Keywords

neural networksadaptive missile autopilotstate-dependent riccati equation

Mathematics Subject Classification ID

Learning and adaptive systems in artificial intelligence (68T05) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51) Adaptive control/observation systems (93C40)

Related Items (2)

A robust state-dependent Riccati equation controller with parameter uncertainty and matched disturbance ⋮ A novel controller for nonlinear uncertain systems using a combination of SDRE and function approximation technique: regulation and tracking of flexible-joint manipulators

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