Isolated satellite surge current detecting method

A technology of inrush current and detection method, applied in the direction of only measuring current, measuring current/voltage, measuring device, etc., can solve the problems of inability to detect inrush current, lack of inrush current detection means for whole star test, etc., and achieve the detection result. Intuitive, to ensure star-to-earth isolation, to ensure the effect of accuracy and safety

Inactive Publication Date: 2017-10-20
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] First, the telemetry sampling frequency on the star is far lower than the frequency required for surge detection, and the surge current cannot be detected
[0005] Second, there is a lack of effective surge current detection means in the whole star test

Method used

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  • Isolated satellite surge current detecting method

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Embodiment Construction

[0017] The preferred embodiments of the present invention are given below in conjunction with the accompanying drawings to describe the technical solution of the present invention in detail.

[0018] Such as figure 1 As shown, the isolated satellite surge current detection method of the present invention comprises the following steps:

[0019] Step 1, clamp the Hall current clamp to the cable harness of the satellite main bus;

[0020] Step 2, connect the output end of the current clamp to a PC (Personal Computer, personal computer) after passing through the signal high-speed sampler;

[0021] Step 3: Compile the upper computer software on the PC side to process and store the received current signal;

[0022] Step 4: Through the human-computer interaction interface on the PC side, comparative analysis of surge current values, real-time display of curves, alarms, etc.

[0023] In the first step, the hall sensor is used to collect the current signal of the satellite's main bu...

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PUM

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Abstract

The invention discloses an isolated satellite surge current detecting method which comprises the following steps of 1, clamping a satellite positive bus-bar cable bundle by means of a Hall current clamp; 2, connecting the output end of the current clamp with a PC through a signal high-speed sampling device; 3, programming upper computer software by the PC end, and processing and storing a received current signal; and 4, through a man-machine interaction interface, performing comparative analysis, curve real-time displaying, alarming and the like on a surge current value by the PC end. The isolated satellite surge current detecting method has advantages of simple operation, comprehensive, accurate and effective data. The man-machine interaction interface is utilized for realizing higher visuality of a detecting result. A Hall sensor is utilized for performing isolated sampling on the current signal of the satellite positive bus-bar, thereby ensuring isolation between a satellite and ground, and realizing high safety and high reliability. Furthermore the method ensures high accuracy and high safety in satellite surge current detection.

Description

technical field [0001] The invention relates to a satellite surge current detection method, in particular to an isolated satellite surge current detection method. Background technique [0002] The satellite system has a lot of equipment and complex load characteristics. Many stand-alone equipment is not a purely resistive load, but a capacitive or inductive load. Especially in order to effectively suppress interference, each device is designed with a power module with a filter circuit to improve the reliability of the device in the interference environment, and the use of the power module makes the device often present a capacitive load, satellite power supply and distribution When the power distribution system powers up each device, a large surge current will be generated, which can cause secondary pollution of the circuit, and will have a great impact on the normal operation of the power distribution circuit and related equipment. [0003] At present, there are usually th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R19/00
CPCG01R19/0092
Inventor 刘政黄业平邓武东曲耀斌张国强龚迪陈占胜赖京
Owner SHANGHAI SATELLITE ENG INST
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