Robust synthesized control of electromechanical actuator for thrust vector system in spacecraft

DOI10.1016/j.camwa.2011.10.026zbMath1322.93078OpenAlexW2037225355MaRDI QIDQ745746

Chenglin Zhu, Yunhua Li, Lu, Hao

Publication date: 14 October 2015

Published in: Computers \& Mathematics with Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.camwa.2011.10.026

zbMATH Keywords

robust controlspacecraft\(H_{\infty }\) controlelectromechanical actuator\(\mu\) synthesispeturbation

Mathematics Subject Classification ID

Application models in control theory (93C95) (H^infty)-control (93B36)

Related Items (2)

Sliding-mode-based robust controller design for one channel in thrust vector system with electromechanical actuators ⋮ Attitude stabilization control of a quadrotor UAV by using backstepping approach

Cites Work

• Stable adaptive fuzzy control for MIMO nonlinear systems

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