2020
DOI: 10.1177/0954410020940882
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Remaining useful life prediction for auxiliary power unit based on particle filter

Abstract: Auxiliary power unit is one of the indispensable systems for civil aviation aircraft but the traditional planned maintenance cannot meet the actual needs of airlines. In this work, the key performance parameters of the auxiliary power unit are selected by using recursive feature elimination method. With the selected parameters, the remaining useful flight cycle of the auxiliary power unit is predicted by applying particle filter techniques. Some improved algorithms such as Gaussian particle filter and auxiliar… Show more

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Cited by 5 publications
(5 citation statements)
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“…Commonly used fusion methods involve Kalman-filter-based and particle-filter-based approaches. Eshwar et al [8] presented an online fatigue life prediction model based on an extended Kalman filter for civil infrastructure applications, while Guo et al [9] successfully predicted remaining effective flight cycles for aircraft auxiliary power units. It is important to note that equipment maintenance decision-making and optimization technology plays a crucial role in reliability engineering.…”
Section: Literature Reviewmentioning
confidence: 99%
See 1 more Smart Citation
“…Commonly used fusion methods involve Kalman-filter-based and particle-filter-based approaches. Eshwar et al [8] presented an online fatigue life prediction model based on an extended Kalman filter for civil infrastructure applications, while Guo et al [9] successfully predicted remaining effective flight cycles for aircraft auxiliary power units. It is important to note that equipment maintenance decision-making and optimization technology plays a crucial role in reliability engineering.…”
Section: Literature Reviewmentioning
confidence: 99%
“…. N , and particle filtering uses a combination of both to represent the state posterior probability distribution [9]:…”
Section: Rul Prediction Based On Particle Filtering Algorithmmentioning
confidence: 99%
“…For instance, as illustrated in Figure 1, the two APUs had already failed when their Exhaust Gas Temperature (EGT) reached the limit. 3 There are obvious scratches on the turbine rotor blades of the APU in Figure 1(a) and the repair cost was US$ 299,759. Corrosion is found obviously on the turbine of the APU in Figure 1(b) and the repair cost was US$ 366,280.…”
Section: Introductionmentioning
confidence: 99%
“…1 Auxillary Power Unit has not received sufficient attention in maintenance due to its relatively low cost and safety requirements compared to main engines. 3 Unlike the main engines, APUs are designed to operate at lower altitudes as per the operational requirements. Therefore, the failure modes of the APU and the monitoring parameters when it fails are not exactly the same as those of main engines.…”
Section: Introductionmentioning
confidence: 99%
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