Optimal attitude takeover control for failed spacecraft based on multi-nanosatellites

DOI10.1016/J.JFRANKLIN.2023.03.037zbMath1516.93183OpenAlexW4362574815MaRDI QIDQ6099853

Qinwen Li, Zhongjie Meng

Publication date: 21 June 2023

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2023.03.037

Mathematics Subject Classification ID

Automated systems (robots, etc.) in control theory (93C85) Orbital mechanics (70M20)

Cites Work

• Inverse optimal design of input-to-state stabilizing nonlinear controllers

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