摘要
介绍了导弹在真空段自由飞行时加速度计的误差模型及其输出脉冲数据的选取与处理。重点探讨脉冲数据的识方法,并通过具体实例说明了该方法的有效性及其应用价值。
Being in vaccum free-flight phase, The error model of the acceierometer and the selection and precessing of its output puise data are intrc-luccd. The identification method of puse data is probed emphapcais The effectiveness and application value of this identification method are expiaincd by example.
出处
《战术导弹技术》
1993年第1期46-51,共6页
Tactical Missile Technology
关键词
面对面导弹
导航
数据辨识
Ground to ground missile Strpdown inertial navigation Accelerometer Error anaivsis Identificanon
