Article ID Journal Published Year Pages File Type
10680857 Acta Astronautica 2014 13 Pages PDF
Abstract
► The paper studies a spinning rigid body under axial thrust and internal motion. ► Its stability is investigated by using linearized equations about a uniform spin. ► We show that the envelope of the stationary solutions is the stability boundary. ► New parametrizations of the stability boundary provide valuable new insights. ► The model is demonstrated by the actual parameters of ESA's Ulysses satellite.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Authors
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