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Aircraft on-orbit test two-way traceability method and equipment

A technology of aircraft and traceability information, applied in the field of communication, can solve problems such as two-way traceability, achieve the effect of strengthening quality control and realizing refined management

Active Publication Date: 2021-06-22
ACAD OF OPTO ELECTRONICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The embodiment of the present invention provides a method and equipment for two-way traceability of aircraft on-orbit tests, which are used to solve the problem of two-way traceability of aircraft on-orbit tests in the prior art

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  • Aircraft on-orbit test two-way traceability method and equipment
  • Aircraft on-orbit test two-way traceability method and equipment
  • Aircraft on-orbit test two-way traceability method and equipment

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Embodiment Construction

[0060] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0061] The on-orbit test of the aircraft requires not only the close cooperation of multiple links on the ground, but also the closed-loop processing of the heaven and earth loop from application, planning, execution to test data release. Limited by the functional performance of the on-orbit vehicle and the capability of the space-ground communica...

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Abstract

Embodiments of the present invention provide a bidirectional traceability method and device for an aircraft on-orbit test. The method includes: using the annotation method and the analytical method to obtain traceability annotations and traceability associated information of each stage of the on-orbit test; based on the traceability annotations and the traceability associated information, perform forward traceability and / or reverse traceability of the on-orbit test. . In the embodiment of the present invention, by combining the annotation method and the analytical method, traceability annotation and traceability association are performed for each stage of the on-orbit test, so as to record and trace the evolution and development process of the application for the on-orbit test of the aircraft, and also record and trace the evolution and development process of the application for the on-orbit test of the aircraft. The entire execution process is recorded and analyzed to realize the refined management of the aircraft on-orbit test, and to provide technical support for strengthening the quality control, risk control, and performance evaluation of the aircraft on-orbit test.

Description

technical field [0001] The invention relates to the field of communication technology, in particular to a two-way traceability method and equipment for an aircraft on-orbit test. Background technique [0002] The basic workflow of the aircraft on-orbit test includes the user submitting a test application to the aircraft operation management center (hereinafter referred to as the "operation management center"), and the operation management center designs and formulates the on-orbit work plan for the aircraft and payloads based on the on-orbit test application submitted by the user. , test instructions, and finally the aircraft and the payload execute the test instructions, complete the technical tests required by the user, and provide the corresponding test data to the user. [0003] With the increase in the number of aircraft, the increase in the payload capacity of the aircraft, and the increase in public participation in the on-orbit test of the aircraft, the number of on-...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F16/22G06F16/2455
CPCG06Q10/103G06F16/22G06F16/2455
Inventor 曲艺王生
Owner ACAD OF OPTO ELECTRONICS CHINESE ACAD OF SCI
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