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 was established when the measurement ... https://www.spidertattooz.com/Messerschmitt-Me262A-1A-Fighter-Aircraft-LT-Walter-Hagenah-III-Jagdeschwader-7-Larz-Airfield-Germany-1945-German-Luft/