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Air vehicle integrated testing system based on 1553B bus

An aircraft and bus controller technology, which is applied in the field of verification of avionics system parameters and characteristics, can solve the problems of poor comprehensive utilization, low reliability, and misoperation by testers, so as to reduce test costs, eliminate repeated use, and prevent errors. effect of action

Active Publication Date: 2014-02-19
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This technology allows for higher integrated testing systems while maintaining their functionality. It uses an improved communication method called CAN (Controller Area Network) instead of just sending signals between devices like sensors. By connecting this new device through a specialized connector, it becomes more effective than previous methods because they only needed two connections - one connection being used when measuring and controlling the flight's altitude level. Additionally, there may also have direct access capabilities such as accessing external databases without requiring any modifications beforehand. Overall, these technical improvements make the current state of affairs even better.

Problems solved by technology

The technical problem addressed in this patented text relates to improving testing efficiency during flight operations after manufacturing or servicing an air space vehicle (AV) without requiring excessive human labor costs associated therewith. Traditional methods involve multiple separate devices connected together through wires, making them challenging to maintain conformance across all types of AV's systems.

Method used

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  • Air vehicle integrated testing system based on 1553B bus

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Embodiment Construction

[0017] Specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0018] Such as figure 1 As shown, the present invention provides an aircraft integrated test system based on 1553B bus, including: power distribution conversion module, DC power supply, DC power supply controller, AC power supply, AC power supply controller, measurement and control computer, bus controller, test Interface adapter, bus protocol conversion module, AD acquisition module, digital multimeter, test control module, signal conditioning module and data interpretation module;

[0019] The external power supply supplies power to the DC power supply and the AC power supply through the power distribution conversion module. The DC power supply controller controls the DC power supply to provide DC power to the test interface adapter. The AC power supply controller controls the AC power supply to provide AC power to the test interface...

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Abstract

An air vehicle integrated testing system based on a 1553B bus comprises a power distribution conversion module, a direct-current power source, a direct-current power source controller, an alternating-current power source, an alternating-current power source controller, a measurement and control computer, a bus controller, a testing interface adapter, a bus protocol conversion module, an AD collecting module, a digital multimeter, a testing control module, a signal conditioning module and a data interpretation module. Related equipment in a traditional air vehicle testing scheme is integrated sufficiently to form a highly integrated general testing platform, and ground testing for an air vehicle achieves integration, miniaturization and portability assisted by advanced software technologies.

Description

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Claims

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Application Information

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Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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