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Descripción
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| The correlation of the Thermal Mathematical Models is often performed manually, and the results obtained in this way are generally not the optimum and could be improved with other strategies. A method of correlation is presented for for steady-state cases. The method is based on a Jacobian matrix formulation and a Moore-Penrose pseudo-inversion. The formulation allows the correlation of a model with several load cases, as it is the usual case in space projects. As an example, it has been applied to the thermal mathematical model of the Optics Unit of the instrument PHI of the ESA Solar Orbiter mission. | |
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Internacional
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Si |
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Nombre congreso
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8th European Conference for Aeronautics and Space Sciences |
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Tipo de participación
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960 |
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Lugar del congreso
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Madrid |
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Revisores
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Si |
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ISBN o ISSN
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DOI
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10.13009/EUCASS2019-649 |
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Fecha inicio congreso
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01/07/2019 |
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Fecha fin congreso
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04/07/2019 |
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Desde la página
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1 |
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Hasta la página
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9 |
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Título de las actas
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8th European Conference for Aeronautics and Space Sciences |