On stability and stabilization of the linearized spacecraft attitude control system with bounded inputs

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Publication:2280726

DOI10.1016/j.automatica.2019.03.011zbMath1458.93200OpenAlexW2939956788WikidataQ128086968 ScholiaQ128086968MaRDI QIDQ2280726

Yanyan Li

Publication date: 19 December 2019

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.automatica.2019.03.011




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