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Design of Integrated Flight Test for Avionics System Based on Test State Point Matrix

  • LI Jing ,
  • ZHANG Xingguo ,
  • CHEN Yu
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  • Chinese Flight Test Establishment, Xi’an 710089, China

Received date: 2019-11-11

  Online published: 2025-05-30

Abstract

With the development of avionics technology and the requirement of operational test, the flight test of avionics system needs to change from the single system verification mode to the system comprehensive verification mode under the condition of comprehensive operation. This paper presents a design method of integrated flight test for avionics system based on test state point matrix. By establishing the constraint conditions of integrated flight test and building the mathematical matrix model of test state point, the auxiliary design of avionics system integrated verification task can be realized, and the efficiency and quality of test can be effectively improved.

Cite this article

LI Jing , ZHANG Xingguo , CHEN Yu . Design of Integrated Flight Test for Avionics System Based on Test State Point Matrix[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020 , 40(1) : 31 -34 . DOI: 10.15892/j.cnki.djzdxb.2020.01.007

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Outlines

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