PDE model-based boundary control of a spacecraft with double flexible appendages under prescribed performance
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DOI: 10.1016/j.asr.2019.09.050
Abstract: Abstract This paper investigates a boundary control scheme of a spacecraft with double flexible appendages under prescribed performance. The flexible spacecraft system comprises a rigid central hub and two flexible appendages regarded as continuum models,… read more here.
Keywords: control; spacecraft; flexible appendages; boundary control ... See more keywords