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某低空自旋导弹中的角速度传感器实际上起着角速度陀螺的作用,但由于这是一种旋转式导弹.固联在弹体上的角速度传感器的摆锤沿着导弹纵轴方向随弹体一起以ω转/秒的速度旋转.因而传感器的结构极其特殊,使它在设计和计算分析上有明显的特点.本文主要解决以下问题:(一)建立角速度传感器的运动方程,说明方程成立的条件:论证角速度传感器输出正比于导弹横向角速度输入的条件.(二)对角速度传感器进行特性分析.(三)分析了角速度传感器解析和变换信息的方式.
The angular velocity sensor in a low-altitude spin missile actually plays the role of angular velocity gyro, but since this is a rotary missile, the pendulum of the angular velocity sensor that is fixed on the projectile moves with the projectile along the longitudinal axis of the missile The speed of ω turn per second, so the sensor structure is very special, it has obvious characteristics in the design and calculation of analysis.This paper mainly addresses the following issues: (a) the establishment of angular velocity sensor equations of motion, indicating the establishment of the equation conditions : Demonstrate that the output of the angular velocity sensor is proportional to the input condition of the transverse velocity of the missile. (2) Analysis of the characteristics of the angular velocity sensor. (3) The way of analyzing and transforming the angular velocity sensor is analyzed.