Three-dimensional low-order fixed-time integrated guidance and control for STT missile with strap-down seeker

DOI10.1016/J.JFRANKLIN.2023.07.028zbMath1521.93128MaRDI QIDQ6053859

No author found.

Publication date: 27 September 2023

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

Mathematics Subject Classification ID

Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05)

Cites Work

• Nonlinear modified bias proportional navigation guidance law against maneuvering targets
• Fuzzy adaptive fault tolerant IGC method for STT missiles with time-varying actuator faults and multisource uncertainties
• Integrated guidance and control with partial state constraints and actuator faults
• Adaptive NN control of integrated guidance and control systems based on disturbance observer

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