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Remaining useful life prediction based on UKF for aircraft structure with fatigue crack
更新时间:2026-10-23
    • Remaining useful life prediction based on UKF for aircraft structure with fatigue crack

    • Vol. 50, Issue 7, Pages: 38-45(2018)
    • DOI:10.11918/j.issn.0367-6234.201709020    

      CLC: TU375.2
    • Published:2018

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  • LUO Bin, LIN Lin, ZHONG Shisheng. Remaining useful life prediction based on UKF for aircraft structure with fatigue crack[J]. 2018, 50(7): 38-45. DOI: 10.11918/j.issn.0367-6234.201709020.

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