Model Sets Interacting Algorithm for Maneuvering Target Tracking in the Presence of Glint Noise

闪烁噪声机动 目标跟踪的模型集交互跟踪算法

Taking the target ′ s maneuvering acceleration target ′ s maneuvering time and target ′ s glint noise into account the switching time from aerodynamic control to compound control is decided .

在考虑目标机动加速度大小、目标机动时刻以及 目标 角 闪烁 的 条件下，确定了拦截弹的控制方式由空气动力切换到复合控制时的切换时间。

The formulas for the target RCS and glint linear deviation are developed by using Poynting vector concept .

利用矢量相干求和及坡印亭矢量概念，导出了 目标RCS和 角 闪烁线偏差公式，并得出了几条特定 轨迹上导引头 跟踪目标的模拟结果。

In radar target tracking system because of the random wandering of the target position the measurement noise is called as glint noise which has a considerable influence on the performance when tracking it .

在雷达目标跟踪系统中由于 目标位置的随机摆动，使得对其位置的量测 伴随 着 闪烁噪声的出现，这种 闪烁噪声会对 目标跟踪的性能产生很大的影响。

Target glint is the main factor which influences tracking and guidance accuracy of terminal guidance radar .

目标 角 闪烁是制约末制导雷达跟踪和命中精度的主要因素。

The computational methods of the radar target 's glint are introduced in this paper .

介绍了 目标 角 闪烁的计算方法。

Maneuvering target tracking algorithms should estimate target motion mode and eliminate influence of glint noise at the same time .

机动目标跟踪算法应同时考虑 目标运动模式变化和 闪烁噪声出现对滤波过程的影响。

This paper presents a tracking algorithm for maneuvering target when the measurement noise is glint noise .

给出了一种量测噪声为 闪烁噪声情况下的 模型 集 交互机动 目标跟踪算法。

Target Tracking based on Particle Filter in Glint Noise Environment

闪烁噪声环境下基于粒子滤波的 目标跟踪

Analysis of the Influence of Target Glint on Surface-to-air Missile 's Kill Efficiency

目标 角 闪烁对地空导弹杀伤效能的影响分析

It has been generally accepted that what the radar measures is not the directions of the target but angular glint errors .

一般认为，雷达事实上并不是在测量 目标的方向，而是在测量 目标的角 闪烁方向。

Sonar Target Glint is the inherent error in the measurement of sonar target direction angle .

声纳 目标 角 闪烁是声纳在对目标方位角进行测量时存在的固有误差。

The line-of-sight rate is analyzed for the influences of the airframe radome effects and target glint . Second the compensation of the miss distance based on trajectory-control lateral-jets is researched .

针对弹体环节、天线罩效应和 目标 角 闪烁噪声等因素，分析了对制导系统视线转率的影响；其次，研究了基于轨控直接侧向力的脱靶量补偿方法。

Influence of Target Glint on the Precision of Guidance and Control

目标 闪烁对制导精度的影响

Then based on the two-dimensional GTD scattering centers model of the missile target the modeling approach to the missile target glint is discussed . Meanwhile the two-dimensional determinate model of glint linear deviation is obtained .

接下来基于某型导弹 目标的二维GTD散射中心模型讨论了该导弹目标的 角 闪烁建模过程，并得到了其角闪烁线偏差的二维确定性模型。

This paper established two models of sonar target glint deviation using the highlight model and plate element method . The glint characteristic of rigid sphere and Benchmark targets was analyzed with these models .

本文分别利用声纳 目标 回波亮点模型与板块元方法建立了声纳 目标 角 闪烁的两种模型，对刚性球及Benchmark目标的角闪烁特征进行了分析。

Next the relevant theory and researching actuality of the radar target glint are summarized .

接下来对雷达 目标 角 闪烁的相关理论及研究现状进行了概括。