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SCPI instruction management method for evaluating spacecraft power supply system

A technology of command management and power supply system, applied in command analysis, electrical digital data processing, instruments, etc., can solve problems such as unproposed solutions

Pending Publication Date: 2021-11-26
BEIJING INST OF SPACECRAFT SYST ENG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the comparison in the related art has not yet proposed an efficient solution

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  • SCPI instruction management method for evaluating spacecraft power supply system
  • SCPI instruction management method for evaluating spacecraft power supply system
  • SCPI instruction management method for evaluating spacecraft power supply system

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Embodiment Construction

[0025] It should be understood that the specific embodiments described here are only used to explain the present disclosure, not to limit the present disclosure.

[0026] In the following description, use of suffixes such as 'module', 'part' or 'unit' for denoting elements is only for facilitating description of the present disclosure and has no specific meaning by itself. Therefore, 'module', 'part' or 'unit' may be used in combination.

[0027] figure 1 A schematic structural diagram of an implementation of a system for evaluating a spacecraft power supply system provided by an embodiment of the present disclosure, as shown in figure 1 As shown, the system includes: a test instrument 10 , a node device 20 , a server 30 and a client 50 . Wherein, the test instrument 10 can be directly connected to the node device 20 , or connected through a switch 40 . The test instrument 10 can be connected to the server 30, and the server 30 has the function of a node device at this time...

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Abstract

The invention relates to an SCPI instruction management method for evaluating a spacecraft power supply system. The method comprises the steps of determining an identifier of an instruction type, an identifier of a test instrument type, an identifier of node equipment, an identifier of a test instrument, an identifier of an SCPI instruction and instruction content of the SCPI instruction; and generating a control command, wherein the information carried by the control command comprises the identifier and the instruction content of the SCPI instruction. The node equipment acquires the control command, and judges whether the control command corresponds to the node equipment according to the identifier of the node equipment in the control command; under the condition that the control command corresponds to the node equipment, determining a test instrument corresponding to the control command according to the identifier of the test instrument in the control command; and sending the instruction content of the SCPI instruction in the control command to the determined test instrument. According to various identifications in the control command, the SCPI instruction is sent to a plurality of types of test instruments and is distinguished.

Description

technical field [0001] The present disclosure relates to the field of spacecraft power system evaluation, in particular to an SCPI command management method used for spacecraft power system evaluation. Background technique [0002] In the test of spacecraft power supply and distribution system, the test scope is wide, including system level, sub-system level, subsystem level, equipment level, module level, component level, etc.; test dimensions are many, including electromechanical thermal interface, electrical performance, reliability Performance, longevity, software engineering, technology maturity, etc. Therefore, computer assistance is introduced to automate the testing process to a certain extent, reduce the time and human resources occupied by the testing work, and further enhance the accuracy and confidence of the testing work. [0003] During the test, it is necessary to send instructions (including but not limited to SCPI instructions) to various and multiple test ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F9/30
CPCG06F9/30003G06F9/30145
Inventor 王超
Owner BEIJING INST OF SPACECRAFT SYST ENG