Manoeuvring and vibration reduction of a flexible spacecraft integrating optimal sliding mode controller and distributed piezoelectric sensors/actuators

DOI10.1002/acs.931zbMath1266.93025OpenAlexW2119935475MaRDI QIDQ5300367

Guangfu Ma, Qinglei Hu

Publication date: 27 June 2013

Published in: International Journal of Adaptive Control and Signal Processing (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/acs.931

zbMATH Keywords

vibration controlflexible spacecraftpiezoceramicspositive position feedback (PPF)optimal sliding mode control

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Variable structure systems (93B12)

Cites Work

• Variable-structure control of spacecraft large-angle maneuvers

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