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- W1562003249 abstract "This paper presents an extension of the method of integral coordinates to the stability analysis of hybrid dynamical systems containing two- and three-dimensional elastic members. A common approach to such problems consists of system discretization by means of series representation in terms of admissible functions, an approach involving lengthy computations. By contrast, the method of integral coordinates yields stability criteria with relative ease and in a form that permits ready physical interpretation. As an application, the attitude stability of a force-free satellite containing a membrane is investigated and closed-form stability criteria are derived." @default.
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- W1562003249 title "Stability Analysis of Flexible Spacecraft via the Method of Integral Coordinates" @default.
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- W1562003249 doi "https://doi.org/10.2514/3.49780" @default.
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