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

作　　者：许飞 袁杰波 田若思 丁小芩 荣婉婷 XU Fei;YUAN Jie-bo;TIAN Ruo-si;DING Xiao-qin;RONG Wan-ting(Shanghai Electro-Mechanical Institute,Shanghai 201109,China;Harbin Institute of Technology,Heilongjiang Harbin 150001,China)

机构地区：[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

出　　处：《现代防御技术》2020年第2期74-80,共7页Modern Defence Technology

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。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.

关 键 词：飞控 动基座对准 桌面测试 收敛品质 通用化 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]