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Spacecraft lithium ion battery cycle life prediction method

A lithium-ion battery, cycle life technology, applied in the direction of instruments, measuring electricity, measuring devices, etc., can solve the problems of poor accuracy, inability to accurately predict the performance degradation curve of lithium batteries, and "capacity regeneration"

Active Publication Date: 2019-09-10
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

[0009] The "capacity regeneration" and fluctuation phenomena of lithium batteries make the performance degradation curve very complicated
Existing traditional time series models (such as autoregressive integrated moving average model) and regression models (such as Gaussian process regression) cannot accurately predict the performance degradation curve of lithium batteries, and they are not sensitive to "capacity regeneration" and fluctuations. Poor forecasting accuracy and other issues

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  • Spacecraft lithium ion battery cycle life prediction method
  • Spacecraft lithium ion battery cycle life prediction method
  • Spacecraft lithium ion battery cycle life prediction method

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Embodiment Construction

[0060] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0061] refer to Figure 1 to Figure 5 , the invention provides a method for predicting the cycle life of a spacecraft lithium-ion battery, comprising the following steps:

[0062] S1: Collect capacity data of lithium-ion batteries ({c 1 , c 2 ,...,c t}), c t Indicates the remaining capacity of the lithium-ion battery in the tth charge-discharge cycle.

[0063] S2: Calculate the time series SOH of the state of health of the lithium-ion battery BAT .

[0064] During t charge and discharge cycles, the state of health value SOH(t) of the lithium-ion battery is:

[0065]

[0066] where c t I...

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Abstract

The invention discloses a spacecraft lithium ion battery cycle life prediction method. The method comprises the following steps: firstly collecting capacity data of a lithium ion battery; computing ahealth state time sequence SOHBAT of the lithium ion battery; decomposing the health state time sequence SOHBAT of the lithium ion battery by applying an empirical mode decomposition model; predictinga global degradation trend of the SOHBAT based on an ARIMA model; predicting the local regeneration and fluctuation of the SOHBAT based on the GPR model; integrating prediction results of the ARIMA model and the GPR model, and acquiring the spacecraft lithium ion battery cyclic life prediction. The global degradation trend and the local capacity regeneration and fluctuation phenomenon of the battery health state time sequence SOHBAT can be effectively extracted by utilizing the empirical mode decomposition method, the global trend and local fluctuation phenomenon of the battery health changecan be simulated by utilizing each of the ARIMA model and the GPR model, the capacity regeneration and fluctuation prediction problem in the battery performance degradation can be effectively solved,so that real health degradation trend of the lithium battery can be captured by integrating the models, and the accuracy of the lithium battery long-term prediction is improved.

Description

technical field [0001] The invention relates to the field of cycle life prediction methods for spacecraft lithium-ion batteries, in particular to a method for predicting the cycle life of spacecraft lithium-ion batteries based on a multi-scale ARIMA and GPR fusion model. Background technique [0002] Spacecraft has important strategic significance for social economy and national defense construction, and it plays an important role in the fields of meteorological observation, resource detection, military reconnaissance, geological exploration and positioning and navigation. The space environment is "dangerous", and various unexpected factors can easily cause abnormalities and failures of spacecraft. At the same time, the mechanical strain caused by the use of the spacecraft, the aging of components, and the performance degradation of the energy storage power supply affect the health of the spacecraft all the time. In the context of the rapid development of contemporary aeros...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/392G01R31/382
CPCG01R31/382G01R31/392
Inventor 张涛刘亚杰雷洪涛黄生俊王锐李国政李训嘉
Owner NAT UNIV OF DEFENSE TECH
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