CAJ | 학술논문

针对高射速小口径舰炮如何进行防空反导的问题，文章论述了未来空域窗的构造和设计，并通过仿真比较不同射击误差协方差矩阵和空域窗半径下的毁伤效能，得出不同射击协方差矩阵和空域窗半径影响了未来空域窗毁伤区域的大小。因此，在保证一定命中概率的前提下，通过调整射击误差协方差矩阵和未来空域窗半径可以有效提高空域窗毁伤区域的大小，从而在目标大范围机动的情况下，保证了舰炮的反导效能。
침대고사속소구경함포여하진행방공반도적문제，문장논술료미래공역창적구조화설계，병통과방진비교불동사격오차협방차구진화공역창반경하적훼상효능，득출불동사격협방차구진화공역창반경영향료미래공역창훼상구역적대소。인차，재보증일정명중개솔적전제하，통과조정사격오차협방차구진화미래공역창반경가이유효제고공역창훼상구역적대소，종이재목표대범위궤동적정황하，보증료함포적반도효능。
Aiming at the anti-missile ability of high firing rate small caliber gun, this paper discusses the design and construction of fu- ture airspace window. Through comparing the efficiency of simulation based on different shooting covariance matrix and airspace window radi- us, the result shows that shooting covariance matrix and airspace window radius affect the size of the damaging area of future airspace win- dow. Therefore, under the premise of ensuring a certain hit probability, adjusting the shooting covariance matrix and the radius of future air- space window can effectively improve the size of the damaging area of future airspace window'. And this method ensures the anti-missile effec- tiveness of high firing rate small-ealiber gun under the large-scale maneuvering situation of target.