Orbit-attitude-vibration coupled dynamics of tethered solar power satellite
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DOI: 10.1016/j.asr.2020.09.036
Abstract: Abstract A new orbit-attitude-vibration coupled dynamic model of the tethered solar power satellite (Tethered SPS) is established based on absolute nodal coordinate formulation. The Hamilton’s equation of the system is derived by introducing generalized momentum… read more here.
Keywords: system; vibration coupled; attitude vibration; tethered solar ... See more keywords