Variable structure controller design for spacecraft nutation damping

DOI10.1109/TAC.1987.1104627zbMath0611.93049OpenAlexW2149685526MaRDI QIDQ3752262

Thomas A. W. III Dwyer, Hebertt Sira-Ramírez

Publication date: 1987

Published in: IEEE Transactions on Automatic Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1109/tac.1987.1104627

zbMATH Keywords

spacecraftVariable structure systemsactive nutation dampingRobust feedback stabilization

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Application models in control theory (93C95) Existence of optimal solutions belonging to restricted classes (Lipschitz controls, bang-bang controls, etc.) (49J30) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (4)

On the decentralized stabilization of interconnected variable structure systems using output feedback ⋮ Robust attitude control of spacecraft using sliding mode control and productive networks ⋮ Differential geometric methods in variable-structure control ⋮ Crew exploration vehicle (CEV) attitude control using a neural–immunology/memory network

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