[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Design of Flight Test for Avionics System Based on Capability
Received date: 2020-02-04
Online published: 2025-02-12
According to the requirements of operational test for avionics system of military aircraft, this paper puts forward the design ideas of the flight test for avionics system, which are based on the analysis of the working characteristics of the equipment from the bottom up and the research of the equipment operation from the top down. According to the analysis of the working characteristics of equipment, this paper expounds three perspectives and specific methods of the analysis of the working characteristics of equipment from the perspective of system engineering, establishes the analysis concept of "complete object", and the formed theory and method have good engineering application significance.
Key words: flight test; capability; avionics system
LI Jing , ZHANG Xingguo , LI Tuo . Design of Flight Test for Avionics System Based on Capability[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020 , 40(3) : 9 -12 . DOI: 10.15892/j.cnki.djzdxb.2020.03.003
| [1] |
孙伟. 武器系统测试性评定方法与试验用例设计[J]. 兵器装备工程学报, 2016, 37(8):52-55.
|
| [2] |
曲宝忠, 于海涛. 海军战术导弹武器系统试验设计[J]. 战术导弹技术, 2001(6):32-40.
|
| [3] |
蒋晓菲. 大数据时代下高校设备全生命周期管理及数据价值的研究[J]. 实验技术与管理, 2016, 33(5): 264-266.
|
| [4] |
周自全. 飞行试验工程[M]. 北京: 航空工业出版社, 2010:358-466.
|
| [5] |
|
| [6] |
汪应洛. 系统工程[M]. 北京: 机械工业出版社, 2010:100-200.
|
/
| 〈 |
|
〉 |