Robust Actuator‐Fault‐Tolerant Control System Based on Sliding‐Mode Observer for Thrust‐Vectoring Aircrafts

DOI10.1002/asjc.1841zbMath1422.93035OpenAlexW2809245908WikidataQ129623299 ScholiaQ129623299MaRDI QIDQ5194831

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Publication date: 17 September 2019

Published in: (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/asjc.1841

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