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A SOC estimation method for UAV power battery in high-altitude flying environment

A mobile power and unmanned aerial vehicle technology, applied in the direction of measuring electricity, measuring electrical variables, instruments, etc., can solve the problems of large amount of data, inability to apply SOC estimation, and difficulty in obtaining parameters, and achieve the effect of a single plane mode

Active Publication Date: 2021-05-11
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, in the calculation process of the above method, some parameters are difficult to obtain, the amount of data is large, and the accurate estimation of the battery SOC is an important parameter for the control of the hybrid propulsion system, so there are certain defects, and it cannot be applied to the power battery of the drone in the high-altitude environment. SOC estimation on

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  • A SOC estimation method for UAV power battery in high-altitude flying environment
  • A SOC estimation method for UAV power battery in high-altitude flying environment
  • A SOC estimation method for UAV power battery in high-altitude flying environment

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[0027] 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.

[0028] SOC estimation method for power battery of UAV in high-altitude flight environment, such as figure 1 shown, including the following steps:

[0029] Step 1: In the ground and high-altitude environment simulation test stage, establish the first form in the data column with temperature, air pressure, and discharge rate as the item column, and the actual total capacity of the battery in the current state, as follows Figure 5 shown. The equipment used in the test includes industrial computer, charge and discharge test platform, and high-altitude environment test box. The specific connections a...

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Abstract

The invention discloses a method for estimating the SOC of a power battery of an unmanned aerial vehicle in a high-altitude flight environment, which includes: first simulating the high-altitude flight environment to establish the item column of temperature, air pressure, and discharge rate, the actual total capacity of the battery in the current state, and the loss of discharge capacity It is the first table and the second table in the data column, and then the actual total capacity and discharge capacity loss of the battery under nominal conditions are obtained by charging and discharging under nominal conditions, and the SOC of the battery during the flight of the drone is calculated. Finally calculate the SOC of the battery after the flight. The invention involves few parameters, simple method and high accuracy.

Description

technical field [0001] The present invention relates to the field of power battery management systems for unmanned aerial vehicles in high-altitude flying environments, in particular to a SOC (State of Charge, state of charge) estimation method for unmanned aerial vehicle power batteries in high-altitude flying environments. Background technique [0002] The SOC state of charge, also known as the remaining capacity, represents the ratio of the remaining capacity of the battery after it has been used for a period of time or left unused for a long time to the capacity of the fully charged state, usually expressed as a percentage. SOC is related to the power battery charging and discharging system, operating temperature and battery health status, and reflects the current remaining power state of the power battery. The commonly used formula is as follows: Since the rated capacity of the battery is not constant, as the battery ages, there is a capacity loss during use, and the c...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01R31/382G01R31/367
CPCG01R31/367G01R31/382
Inventor 李玉芳徐国放赵万忠任陈
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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