摘要
针对比例导引律及其许多改进方法不能预测大机动目标因机动飞行引起的方位变化的缺陷,本文研究了一种新型的对干扰进行补偿的预测拦截方法.通过介绍初始扰动和常驻外扰动的估算方法并利用不变性原理对其进行补偿,视线角速度基本稳定在零点附近,达到了预测拦截、提高攻击大机动目标制导精度的目的.
In order to make up the weakness that the Proportional Navigation Guidance (PNG) and its improved guidance laws can't predictively intercept the position change caused by target's high maneuver. a new predictive intercept guidance law which compensates the disturbace is studied. This paper introduces the initial disturbance and the estimation method of existed external disturbance in a navigation system and compensating it through the principle of in-variability. The simulation results show that the LOS angle rate is almost kept at a low va-lue, and the purposes of predictive intercept and the improvement of guidance precision have been reached in attacking highly maneuvering targets.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1994年第2期127-131,共5页
Journal of Beijing University of Aeronautics and Astronautics
关键词
导弹
制导
扰动补偿
反导弹导弹
guided missile guidance
intercept trajectories
disturbances compensation
predictive intercept