飞控动基座对准性能桌面测试系统设计

doi:10.3969/j.issn.1009-086x.2020.02.013

现代防御技术 ›› 2020, Vol. 48 ›› Issue (2): 74-80.DOI: 10.3969/j.issn.1009-086x.2020.02.013

飞控动基座对准性能桌面测试系统设计

许飞¹, 袁杰波¹, 田若思¹, 丁小芩¹, 荣婉婷²

1.上海机电工程研究所,上海 201109;
2.哈尔滨工业大学,黑龙江哈尔滨 150001

收稿日期:2019-07-31 修回日期:2019-09-08 出版日期:2020-04-20 发布日期:2021-01-20
作者简介:许飞(1992-),男,江苏盐城人。助工,硕士,主要研究领域为软件设计开发。通信地址:201109 上海市元江路3888号上海机电工程研究所十八室 E-mail:xflwtg@163.com

Design of Desktop Test System for Flight Control Dynamically Pedestal Alignment

<a href="https://www.xdfyjs.cn/EN/article/advancedSearchResult.do?searchSQL=(((XU Fei[Author]) AND 1[Journal]) AND year[Order])" target="_blank">XU Fei</a>1,<a href="https://www.xdfyjs.cn/EN/article/advancedSearchResult.do?searchSQL=((( YUAN Jie-bo[Author]) AND 1[Journal]) AND year[Order])" target="_blank"> YUAN Jie-bo</a>1,<a href="https://www.xdfyjs.cn/EN/article/advancedSearchResult.do?searchSQL=((( TIAN Ruo-si[Author]) AND 1[Journal]) AND year[Order])" target="_blank"> TIAN Ruo-si</a>1, DING Xiao-qin1 RONG Wan-ting2

1. Shanghai Electro-Mechanical Institute,Shanghai 201109,China;
2. Harbin Institute of Technology,Heilongjiang Harbin 150001,China

Received:2019-07-31 Revised:2019-09-08 Online:2020-04-20 Published:2021-01-20

摘要/Abstract

摘要： 针对飞控动基座对准因为外部信息不断变化导致性能测试无法覆盖动态过程的问题,提出了一种基于MFC和Matlab语言开发的飞控动基座对准性能桌面测试系统。该系统具备设置测试环境、测试首次收敛时间、评估收敛品质、测试导航误差等功能。通过更换Matlab数字仿真动态库文件,可实现动基座对准桌面测试的通用化。

关键词: 飞控, 动基座对准, 桌面测试, 收敛品质, 通用化

Abstract: Contraposed the problem that flight control dynamically pedestal alignment can not test the overall dynamic process because of the constantly changing external information, a kind of desktop test system for flight control dynamically pedestal alignment based on MFC and Matlab technology was proposed. The system has multiple functions such as test environment setting, first convergence testing, convergence quality assessment, navigation error testing. By replacing dll dynamic-link library file of Matlab digital simulation, it can achieve universalization of flight control dynamically pedestal alignment.

Key words: flight control, dynamically pedestal alignment, desktop test, convergence quality, universalization

中图分类号:

TJ765.2

许飞, 袁杰波, 田若思, 丁小芩, 荣婉婷. 飞控动基座对准性能桌面测试系统设计[J]. 现代防御技术, 2020, 48(2): 74-80.

XU Fei, YUAN Jie-bo, TIAN Ruo-si, DING Xiao-qin RONG Wan-ting. Design of Desktop Test System for Flight Control Dynamically Pedestal Alignment[J]. Modern Defense Technology, 2020, 48(2): 74-80.

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飞控动基座对准性能桌面测试系统设计

Design of Desktop Test System for Flight Control Dynamically Pedestal Alignment

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