Design of the microsatellite attitude control system using the mixed method via LMI optimization

DOI10.1155/2013/257193zbMath1296.93144OpenAlexW2006369204WikidataQ59025270 ScholiaQ59025270MaRDI QIDQ460362

Erberson Rodrigues Pinheiro, Luiz Carlos Gadelha De Souza

Publication date: 13 October 2014

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2013/257193

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)

Related Items (1)

Uncertainty and disturbance-observer based robust attitude control for satellites

Cites Work

• Using of H-infinity control method in attitude control system of rigid-flexible satellite
• LQG control with an H/sup infinity / performance bound: a Riccati equation approach
• Mixed H/sub 2//H/sub infinity / control: a convex optimization approach
• Linear Matrix Inequalities in System and Control Theory

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