火箭弹投弹偏差修正方法

Windage Modification Method for Rocket Projectile

提出一种火箭弹投弹偏差修正方法,以期进一步提升精准水平。基于火箭弹投弹过程的分析,表明弹着点的固有误差能够被抑制。结合算例提出偏差修正原理和设计思路,并付诸实践。该方法仅需对机载软件进行更改,无需改变机上设备硬件和外部交联关系。方法的有效性通过仿真分析得以验证,将进一步带动火箭弹投放精度的提高。

A windage modification method is proposed for rocket projectile,to further enhance the precise level.Based on the process analysis of rocket projectile,it is deduced that the inherent error of impact point can be suppressed.The windage modification principle and design idea are put forward combined with an example and put into practice.The method only needs to change the airborne software without changing the equipment hardware and the external cross-linking relationship.The effectiveness of such a method is verified by simulation analysis,which will further improve the precision of rocket projectile.