CMPASS Dataset

Citation Author(s):
mingyue
Wu
Submitted by:
mingyue Wu
Last updated:
Tue, 03/25/2025 - 09:36
DOI:
10.21227/q7b4-fs93
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Abstract 

This paper introduces an aircraft engine remaining life prediction model based on an improved Transformer architecture (SBi-Transformer), addressing the computational inefficiencies and inadequate local temporal dependency capturing capabilities of the standard transformer model in processing long sequence data. The SBi-Transformer employs a dual-layer attention mechanism to reduce computational complexity and enhance local temporal dependencies. It eliminates the decoder component, directly using BiLSTM to model the time series of the encoder outputs, supplementing local temporal context information, and strengthening the forward and backward dependency modeling of degradation trends. Ultimately, the integrated global-local features are mapped to remaining useful life (RUL) prediction values through a fully connected layer. Experiments on NASA’s C-MAPSS dataset demonstrate that SBi-Transformer surpasses existing methods in prediction accuracy and uncertainty estimation. Ablation experiments validate the synergistic effects of the modules, indicating that the sparse attention mechanism and BiLSTM complementarily enhance model performance. The model exhibits strong adaptability and generalizability under complex operating conditions and multiple fault modes, with prediction result confidence intervals dynamically converging to the true degradation trajectory. This study provides an efficient and accurate solution for predicting the remaining life of aircraft engines, holding significant engineering application value

      

Instructions: 

To validate the effectiveness of the methods in this chapter, this section uses the C-MAPSS dataset provided by NASA to test the algorithm. This dataset consists of extensive simulated experiments on the degradation processes of critical components in turbofan engines and is publicly available. It is widely used in the problem of predicting the RUL of aircraft engines. The dataset includes four subsets, each recording data from 21 sensors under different operating conditions and fault modes of the simulated turbofan engines. Each subset is divided into a training set and a test set, as shown in Tab.1.

Tab.1. C-MAPSS Dataset

 

Dataset

FD001

FD002

FD003

FD004

Engine units for training

100

260

100

249

Engine units for testing

100

259

100

248

Operating conditions

1

6

1

6

Fault modes

1

1

2

2

Training samples (default)

17731

48819

21820

57522

Testing samples

100

259

100

248

      

Dataset Files

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