Hybrid control of attitude maneuver and structural vibration for a large phased array antenna satellite

DOI10.1016/J.JFRANKLIN.2023.11.049OpenAlexW4389521267MaRDI QIDQ6190549

Unnamed Author, Dongfang Zhu, Xiang Liu, Guangyu Lu, Guo-Ping Cai

Publication date: 6 February 2024

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2023.11.049

zbMATH Keywords

active vibration controlattitude maneuverrigid-flexible coupling dynamic modelcable actuatorslarge antenna satellite

Mathematics Subject Classification ID

Random vibrations in mechanics of particles and systems (70L05) Orbital mechanics (70M20) Control/observation systems governed by functional relations other than differential equations (such as hybrid and switching systems) (93C30)

Cites Work

• Vibration control of a membrane antenna structure using cable actuators
• Agile attitude maneuver with active vibration-suppression for flexible spacecraft
• Nonquadratic cost and nonlinear feedback control
• Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
• Aperiodic Arrays for Spaceborne SAR Applications

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