Software Design of Test System for Missile Flight Control System

被引：0
|
作者：
Chen, Danqiang [1 ,2 ]
Cao, Guohua [1 ]
Fan, Huilin [2 ]
Wang, Jinghua [2 ]
Qi, Duo [2 ]
机构：
[1] Changchun Univ Sci & Technol, Changchun, Jilin Province, Peoples R China
[2] Aviat Univ Air Force, Changchun, Jilin Province, Peoples R China
来源：
INDUSTRIAL INSTRUMENTATION AND CONTROL SYSTEMS, PTS 1-4 | 2013年 / 241-244卷
关键词：
Test system; flight control system; software design; software anti-jamming technique;
D O I：
10.4028/www.scientific.net/AMM.241-244.2764
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Before final assembly and while debugging a missile, in order to ensure the flight control system can work stably and reliably, it is necessary to develop an auto test system. Test software is an important part of the test system. After describing the composition and working principle of the flight control system, summarizing the test requirements, the test software is designed. The design ideas, test algorithm, realization and key technologies, software anti-jamming techniques are introduced in detail. The test software guarantees the test system test the flight control system generally and reliably.
引用
收藏
页码：2764 / +
页数：2
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