Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/37808
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dc.contributor.authorGoncharenko, Andriy Viktorovichen
dc.date.accessioned2019-02-20T07:25:36Z-
dc.date.available2019-02-20T07:25:36Z-
dc.date.issued2018-10-10-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/37808-
dc.description.abstractThe third part of the generalization for the degrading state maximal probability determination in the framework of the hybrid-optional functions entropy conditional optimality doctrine initiated in the preceding reports was presented in the given report. The issue will be continued with a following sequence of reports.en
dc.language.isoenen
dc.titleAeronautical engineering degrading state maximal probability determination as a proof for the hybrid-optional functions entropy conditional optimality doctrine applicationen
dc.typeArticleen
Appears in Collections:The 8th World Congress, 2018

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