SUCCESSFUL FLUTTER CATHETER ABLATION THROUGH THE AZYGOS CONTINUATION DUE TO AN INTERRUPTED INFERIOR VENA CAVA




Prediction of remaining useful life time of aero engine based on the Wiener process of three-source uncertainty

Given the problem of three-sources uncertainty in aero engine degradation process and the assumption of normal distribution of measurement error in existing research, a Wiener process aero engine residual useful life time(RUL) prediction method with logistic distribution of measurement error was proposed.Firstly, the performance degradation model w

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