Rocket health degree evaluation method based on long-short-term memory auto-encoder

A long-short-term memory and autoencoder technology, which is applied in neural architecture, biological neural network model, design optimization/simulation, etc., can solve the internal connection of dynamic response engines, engine process differences cannot be well matched, and engine operating conditions Diagnose problems such as low reliability of results, achieve the effect of troubleshooting measurement faults and realizing health evaluation

Active Publication Date: 2020-12-11
SHANGHAI AEROSPACE SYST ENG INST
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Problems solved by technology

The current mainstream detection methods mainly include parameter threshold detection, mathematical model prediction, etc. These methods rely on the fixed model coefficients of each engine component, which cannot dynamically reflect the internal relationship between various engine parameters, and cannot be very sensitive to the differences in different engine processes. Good matching, the reliability of the diagnosis result of the engine working condition is low, which is not enough to be used as the basis for the rocket to judge whether the power is abnormal or not

Method used

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  • Rocket health degree evaluation method based on long-short-term memory auto-encoder
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  • Rocket health degree evaluation method based on long-short-term memory auto-encoder

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Embodiment 1

[0050] A rocket health assessment method based on long short-term memory autoencoder. This method takes advantage of the long-short-term memory unit to process time-series data, combines the self-encoder for unsupervised learning, automatically extracts the features of the original data during the normal startup process of the rocket, restores them to realize the abnormal monitoring of the rocket, and combines the health degree calculation function. health estimate. Specifically include the following steps:

[0051] 1. Preprocess multiple data samples X of the raw data of each sensor in the rocket and obtain and keep the preprocessing parameter X max ,X min .

[0052] The preprocessing step is divided into two steps: normalization and data format modification.

[0053] The standardization adopts the min-max standardization method, namely:

[0054]

[0055] Where x' is the data sample after normalization, x is the data sample before normalization, and x min is the smal...

Embodiment 2

[0067] Such as figure 1 As shown, this embodiment relates to a rocket health evaluation system based on long short-term memory autoencoder, including: a data input module, a sample training module, and a data monitoring module. Among them: the data input module is used to input the key raw data of the rocket engine and initially change the data format to meet the input requirements of the long-short-term memory unit; the sample training module uses the sample data to train the model, updates the parameters and saves the final trained model parameters; the data The detection module uses the trained model to monitor the data in real time, draw the data curve, and display the real-time health of the data.

[0068] The raw data is engine performance data.

[0069] Such as figure 2 with image 3 As shown, this embodiment relates to a method for diagnosing the health of a launch vehicle engine based on the above system, which specifically includes the following steps:

[0070] ...

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Abstract

A rocket health degree evaluation method based on a long-short-term memory auto-encoder belongs to the technical field of engine health diagnosis, and comprises the following steps: taking a long-short-term memory unit as a basic unit for constructing a network model, constructing a model by taking the auto-encoder as a framework, performing compressed encoding on original data, performing decoding, and comparing with the original data, and judging the data health degree through the error level between the two. According to the method, the model of the long-short-term memory auto-encoder is adopted to train the ground data, the obtained model can be used for engine data diagnosis in the rocket flight process, measurement faults can be effectively eliminated through verification of historical flight data, the diagnosis accuracy is larger than 95%, the false alarm rate is lower than 5%, and health degree evaluation can be accurately achieved.

Description

technical field [0001] The invention relates to a training method for a launch vehicle engine health diagnosis model based on a long-short-term memory autoencoder, and belongs to the technical field of engine health diagnosis. Background technique [0002] Aerospace has always been a very important sector in my country's strategic deployment, and the rocket engine, which is the power source of aerospace, is even more important. In the rocket launch mission, engine performance and engine thrust play a decisive role in the launch process. How to evaluate the engine health status in an efficient and reliable way during the launch process is the key to the redundant control of rocket power. The current mainstream detection methods mainly include parameter threshold detection, mathematical model prediction, etc. These methods rely on the fixed model coefficients of each engine component, which cannot dynamically reflect the internal relationship between various engine parameters,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06N3/04
CPCG06F30/27G06N3/049G06N3/045
Inventor 谢立张元明绍硕黄兴张婷婷程程况羿王伟哲
Owner SHANGHAI AEROSPACE SYST ENG INST
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