Attitude tracking control of flexible spacecraft with large amplitude slosh

DOI10.1007/S10409-017-0700-9zbMath1390.93587OpenAlexW2614569827MaRDI QIDQ1637979

Mingle Deng, Bao-Zeng Yue

Publication date: 12 June 2018

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-017-0700-9

zbMATH Keywords

flexible spacecraftattitude trackingadaptive sliding mode controldynamic couplinglarge amplitude liquid slosh

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40) Variable structure systems (93B12) Hydro- and aero-acoustics (76Q05)

Related Items (1)

Attitude control of spherical liquid-filled spacecraft based on high-order fully actuated system approaches

Cites Work

• Chaotic attitude and reorientation maneuver for completely liquid-filled spacecraft with flexible appendage
• Heteroclinic bifurcations in attitude maneuver of coupled slosh-spacecraft with flexible appendage
• Coupling dynamic analysis of spacecraft with multiple cylindrical tanks and flexible appendages
• Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel
• Variable-structure control of spacecraft large-angle maneuvers
• Capillary surfaces in an exotic container: results from Space experiments

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