Non-fragile guaranteed cost control for robust spacecraft orbit transfer with small thrust

DOI10.1093/imamci/dnr024zbMath1243.93027OpenAlexW1970493066MaRDI QIDQ5390178

Xiang-Yu Gao, Guang-Ren Duan, Kok Lay Teo

Publication date: 27 April 2012

Published in: IMA Journal of Mathematical Control and Information (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1093/imamci/dnr024

zbMATH Keywords

uncertain systemlinear matrix inequalities (LMIs)guaranteed cost controlinput constraintspacecraft orbit transfer

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Controllability (93B05) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (3)

Robust H_∞ dynamic output feedback control for spacecraft rendezvous with poles and input constraint ⋮ Legendre cooperative PSO strategies for trajectory optimization ⋮ Non-fragile robustH_∞control for uncertain spacecraft rendezvous system with pole and input constraints

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