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Lithium battery on-orbit management simulation test method and device

A technology for lithium batteries and battery packs, applied in the field of lithium battery on-orbit management simulation test methods and devices, can solve problems such as complex software logic

Pending Publication Date: 2021-01-29
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the same time, the voltage difference of the battery pack must be controlled within a certain range, and the power control software must complete the lithium-ion battery voltage measurement and battery equalization processing functions through the battery pack interface management unit; and the software has many functions such as fault detection and overvoltage protection. , the software logic is extremely complex

Method used

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  • Lithium battery on-orbit management simulation test method and device
  • Lithium battery on-orbit management simulation test method and device
  • Lithium battery on-orbit management simulation test method and device

Examples

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Embodiment Construction

[0084] refer to figure 1 , shows a flow chart of the steps of a lithium battery on-orbit management simulation test method provided by an embodiment of the present invention, as shown in figure 1 As shown, the lithium battery on-orbit management simulation test method may specifically include the following steps:

[0085] Step 101: Compare the binding value corresponding to the lithium-ion battery pack management software with the expected value, and determine whether the binding value is consistent with the expected value.

[0086] In this embodiment, the binding value refers to the initial parameter of the lithium-ion battery pack management software after power-on, that is, the initial value of the software after power-on.

[0087] In the stage of ground comprehensive testing, comprehensive lithium battery performance verification and lithium-ion battery pack management software logic verification are the keys to ensure the battery's in-orbit service life and satellite saf...

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Abstract

The invention provides a lithium battery on-orbit management simulation test method and device. The method comprises the following steps: comparing a binding value corresponding to lithium ion storagebattery pack management software with an expected value, and determining whether the binding value is consistent with the expected value or not; when it is determined that the binding value is consistent with the expected value, executing a preset control instruction on the lithium ion storage battery pack management software to verify the accuracy degree of software logic corresponding to the lithium ion storage battery pack management software; under the condition that the accuracy degree is determined to meet the preset condition, the simulation of the lithium ion storage battery pack management software in different modes is realized by adjusting the parameters of a power supply controller; and verifying whether the lithium ion storage battery pack management software and the batteryperformances of the lithium ion storage battery pack meet on-orbit use requirements or not according to a simulation result. According to the invention, the control of the voltage difference between the single bodies in the charging period of the lithium ion storage battery pack is realized, the whole testing process can be programmed by using automatic software, and the testing efficiency and theautomation level are improved.

Description

technical field [0001] The invention relates to the technical field of spacecraft ground testing, in particular to a lithium battery on-orbit management simulation test method and device. Background technique [0002] For the first time, Dongsan B platform uses lithium-ion battery packs as energy storage power sources. During different orbital stages during the satellite service, the battery pack needs to be charged, discharged, and equalized to meet the energy demand of the satellite. [0003] During the orbit light period, the solar battery array charges the lithium-ion battery pack through the power controller, and the lithium-ion battery converts electrical energy into chemical energy and stores it; can be converted into electrical energy. Lithium-ion battery packs have the characteristics of light weight and large specific energy. However, when charging and discharging a lithium-ion battery pack, there are high requirements for charging and discharging current, ambie...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/396G01R31/367
CPCG01R31/396G01R31/367
Inventor 张晓明李斐李晓梦焦荣惠王爽韩欢安然
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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