Airplane management computer software verification environment system

By designing an aircraft management computer software verification environment system, including multiple test equipment and network structures, the problem of inefficiency of traditional verification methods is solved, the need for simultaneous verification of multiple airborne finished products is realized, and verification efficiency and operation simplicity is improved.

CN119829404AActive Publication Date: 2025-04-15CHENGDU KAIDI FEIYAN TECH CO LTD
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Patent Information

Application Number
CN202411904591.5
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-12-23
Publication Date
2025-04-15
Estimated Expiration
2044-12-23

AI Technical Summary

Technical Problem

The traditional aircraft management software verification method is inefficient, and it is necessary to rearrange the system joint commissioning and testing environment, and the operation is complicated and there is a lack of a standard fixed paradigm, resulting in increased work efficiency and workload.

Method used

Design an aircraft management computer software verification environment system, including VMC comprehensive testing equipment, bus network node simulation equipment, bus data acquisition and analysis equipment, and development and comprehensive testing equipment, build Ethernet, reflective memory network and bus network, and provide a standard fixed paradigm and system joint debugging and verification environment.

Benefits of technology

The requirement of multiple airborne finished products to be verified simultaneously by aircraft management software, improve verification efficiency, reduce workload, and provide a standard operating paradigm, simplifying the operating process of staff.

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Abstract

The invention provides an aircraft management computer software verification environment system, and relates to the technical field of equipment testing. The system comprises VMC comprehensive test equipment, bus network node simulation equipment, bus data acquisition and analysis equipment and development and comprehensive test equipment, and an Ethernet, a reflective memory network and a bus network which are used in the system are constructed; wherein the Ethernet, the reflective memory network and the bus network are used in the system for data interaction and equipment control, and the operation of each test equipment is integrated and fixed through the verification environment cabinet, the verification environment finished product cabinet and the verification environment workbench, so that a worker does not need to sort the current environment architecture, and the test efficiency is improved. Therefore, the operation can be carried out at the position of the test equipment to be used in the corresponding functional area. According to the method, the requirement that multiple airborne finished products are subjected to aircraft management software verification at the same time is met, a standard fixed normal form of aircraft management software verification is achieved, and a system joint debugging and joint test verification environment of the airborne finished products is provided.
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