Abstract
Satellites have gained much attention in the past decades for the purpose of remote sensing, communication and so on [8,9,10]. Considering a complex environment and space mission constraints, flexible satellite characterized by light weight structure, limitation of mass, low energy consumption and reduced launch cost, are widely used. Flexible satellites usually consists of a central rigid hub and long flexible appendages such as solar panels.
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Liu, Z., Liu, J. (2020). PDE Modeling and Basic Vibration Control for Flexible Satellite. In: PDE Modeling and Boundary Control for Flexible Mechanical System. Springer Tracts in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-2596-4_3
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DOI: https://doi.org/10.1007/978-981-15-2596-4_3
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