An optimal dynamic output feedback controller for a flexible spacecraft

DOI10.1002/OCA.4660110105zbMath0693.93087OpenAlexW2030826870WikidataQ126238417 ScholiaQ126238417MaRDI QIDQ3469023

M. Seetharama Bhat, Shashi K. Shrivastava, A. G. Sreenatha

Publication date: 1990

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.4660110105

zbMATH Keywords

flexible spacecrafttime-invariantdynamic controllerlow-order dynamic output feedback controllermodified linear quadratic Gaussian (LQG) theory

Mathematics Subject Classification ID

Application models in control theory (93C95) Discrete-time control/observation systems (93C55) Linear systems in control theory (93C05) Optimal stochastic control (93E20) Orbital mechanics (70M20)

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