摘要
试验鉴定中需要基于半实物仿真测试环境测试分析导弹制导控制系统的抗干扰性能,现阶段干扰方案的设计繁多且缺乏科学性,不便于指导武器装备的鉴定验收工作。该文采用正交分析的方法设计抗干扰测试方案,利用导弹制导控制系统数学模型分析各个干扰因素对脱靶量的具体影响,根据分析的结果合理设置正交因素的水平值,以较少的测试方案反映出更加全面的测试信息。利用该测试方案可以减少导弹制导控制系统的测试时间,节约经费,并较好地反映出了导弹制导控制系统的真实抗干扰能力,便于武器装备的定型和验收。
In the test appraisal, it is necessary to analyze and test the anti-jamming performance of the missile guidance control system based on the semi-physical simulation test environment test. At present, the design of the interference plan is numerous and scientifically inconvenient to guide the appraisal and acceptance work of the weapons and equipment. In this paper, orthogonal test method is used to design anti-jamming test scheme.The mathematical model of missile guidance system is used to analyze the influence of each interference factor on the amount of miss distance. According to the result of the analysis, the level of orthogonal factor is set reasonably. Reflect a more comprehensive test information. The test program can reduce the test time of missile guidance control system, save money, and better reflect the true anti-jamming capability of missile guidance control system to facilitate the setting and acceptance of weapons and equipment.
作者
马金龙
马立元
方丹
徐帅
MA Jinlong;MA Liyuan;FANG Dan;XU Shuai(Shijiazhuang Campus of the Army Engineering University,Shijiazhuang 050003,China)
出处
《中国测试》
CAS
北大核心
2019年第3期24-29,共6页
China Measurement & Test
关键词
抗干扰
试验鉴定
正交分析
制导控制
anti-jamming test
test evaluation
orthogonal analysis
guided control
