摘要
建立动基座条件下反舰导弹捷联惯导系统误差传播方程,分析发射平台导航参数误差对导弹惯导定位误差的影响,得出了相关的结论。研究结果可以为武器试验鉴定工作提供支撑。
Based onthe error propagation equation of the strapdown inertial navigation system of the anti ship missile under the condition of moving base,the influence of the navigation parameters of the launching platform on the positioning error of missile inertial navigation system is analyzed, and the related conclusion is drawn.The results of the study can provide support for the weapon test and appraisal work.
出处
《电子测试》
2016年第6X期53-54,共2页
Electronic Test
关键词
发射平台
反舰导弹
捷联惯导系统
launch platform
anti ship missile
strapdown inertial navigation system
