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Simulation test system of star software based on virtual instrument technology

A technology of star service software and simulation test, applied in the field of star service software simulation test system based on virtual instrument technology, can solve the problems of long development cycle and poor versatility, and achieve the effect of short development cycle, strong versatility and convenient operation

Active Publication Date: 2015-09-09
SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Aiming at the limitations of the existing test system, the technical problem to be solved by the present invention is to provide a general test system for multi-model star service software, to meet the fast and efficient software test requirements, and to solve the problems of poor versatility and long development cycle of the existing test system

Method used

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  • Simulation test system of star software based on virtual instrument technology
  • Simulation test system of star software based on virtual instrument technology
  • Simulation test system of star software based on virtual instrument technology

Examples

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example 1

[0033] Such as figure 2 As shown, it is a structural diagram of a star service software simulation test system according to an embodiment of the present invention. The whole simulation test system includes PXI industrial computer, PXI-6259 board card 2, two PXI6624 board cards 3, PXI-8431 serial port card 4, PXI-8464 CAN bus card 6 and PXI-7813rFPGA high-speed transmission card 5, these board cards pass The PXI bus is connected with the industrial computer to form the hardware environment of the star software simulation test system. Each software module based on virtual instrument technology can include 11, respectively: star-arrow separation module 7, direct remote control module 8, analog telemetry module 9, remote control injection number module 10, telemetry receiving and analysis module 11, program-controlled instruction receiving module 12. GPS whole second signal module 13, time reference module 14, CAN data simulation module 15, data transmission module 16 and serial...

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Abstract

The invention relates to a satellite signal simulation technology and a virtual instrument technology, and discloses a housekeeping software simulation test system based on technology of a virtual instrument. The housekeeping software simulation test system comprises an industrial personal computer, an analog / digital signal input and output card, a serial port card, a CAN (Controller Area Network) bus card, and an FPGA (Field Programmable Gate Array) high-speed transmission card, wherein the industrial personal computer is connected with the cards, and the cards are connected with a housekeeping computer. The simulation test system functionally comprises a satellite separation module, a direct remote control module, an analog quantity telemetering module, a remote control digital input module, a telemetering reception and analysis module, a programmable command receiving module, a GPS (Global Position System) second signal module, a time reference module, a CAN data simulation module, a data transmission module and a serial port communication module. The housekeeping software simulation test system is formed by frame type hardware, and is programmed by the flexible software modules. Compared with the prior art, the housekeeping software simulation test system has the beneficial effects of being simple in structure, convenient to operate, short in development period, being widely suitable for various types of housekeeping software, and meeting flexibly-changed dynamic tests and nonstandard signal tests.

Description

technical field [0001] The invention relates to a simulation test system for star mission software, in particular to a simulation test system for star mission software based on virtual instrument technology. Background technique [0002] Due to the high reliability requirements of aerospace equipment, and the reliability and robustness of equipment software are the key factors for its ability to operate well in harsh environments, the key software of these aerospace equipment must undergo strict comprehensive testing before leaving the factory . [0003] At present, many software evaluation agencies in China mainly use two methods for software testing. First, the designer's joint test environment is used instead of the self-developed test bench for software testing. This method cannot perform fault case testing, change the peripheral environment, and cannot conduct comprehensive third-party independent testing. Second, to develop a matching test bench for a single software...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F11/36
Inventor 云颖宋雷军沈炳华赵小军魏冬冬
Owner SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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