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METHOD FOR SURVEY OF SINGLE-POSITION TRILATERATION INCOHERENT RADAR RANGING OF AERIAL TARGETS

机译:航空目标单点三角测量不连续雷达测距的方法

摘要

FIELD: radio equipment.;SUBSTANCE: invention relates to radio engineering and can be used in ground-based systems of active survey single-position radar for detection and location, motion parameters and trajectories of air targets moving in space. To achieve technical result, movement of each air target is considered as a sequence of movements along polyhedral surface approximating to beam specified by vector of inclined range of target. To form trilateration system, auxiliary points B are used on abscissa and D on ordinate axes spaced by distance d from coordinate origin, and calculating range values R from them to the target, rectangular coordinates of the targets, forming the size of the target selection zones by range and angular coordinates. At repeated survey, values of inclined distances, azimuths and angles of targets are measured, and new samples are identified to initial sections of trajectories of previously detected targets. Values and coordinates are calculated for each tracked target. Using extrapolated values of rectangular coordinates from outputs of Kalman filters for formation of selection zones in points Ak+2 of trajectories of targets. Based on the results of subsequent surveys, trajectories of targets are detected by the criterion "three of three", values of distances traveled by targets during the time of scanning, modules of velocity vectors and spatial course angles, as well as flight altitudes and diving or pitch-up angles are calculated. In subsequent surveys coordinates of targets are measured and tracking and construction of their trajectories.;EFFECT: more accurate determination of parameters of movement and trajectories of the located aerial targets.;1 cl, 2 dwg
机译:技术领域本发明涉及无线电工程,并且可以在主动测量单位置雷达的地面系统中用于检测和定位,在空间中移动的空中目标的运动参数和轨迹。为了获得技术效果,每个空中目标的运动被视为沿着多面体表面的运动序列,近似于目标倾斜范围矢量所指定的光束。为了形成三边测量系统,在横坐标上使用辅助点B,在与坐标原点相距d的坐标轴上使用D,并计算从它们到目标的范围值R,目标的直角坐标,形成目标选择区的大小通过范围和角度坐标。在重复测量中,测量目标的倾斜距离,方位角和角度的值,并从先前检测到的目标的轨迹的初始部分中识别出新的样本。为每个跟踪目标计算值和坐标。利用卡尔曼滤波器输出的直角坐标外推值在目标轨迹的点A k + 2 上形成选择区域。根据后续调查的结果,通过“三分之三”标准检测目标的轨迹,扫描期间目标行进的距离值,速度矢量和空间航向角的模块以及飞行高度和俯冲或俯仰角的计算。在随后的勘测中,测量目标的坐标并跟踪和构建其轨迹。效果:更精确地确定所定位的空中目标的运动和轨迹参数。1cl,2 dwg

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