首页> 外国专利> METHOD TO SUPPORT GROUP AIR TARGETS OF 'AIRCRAFT WITH TURBOJET' CLASS IN RADAR LOCATION STATION AT EXPOSURE OF RATE INTERFERENCE

METHOD TO SUPPORT GROUP AIR TARGETS OF 'AIRCRAFT WITH TURBOJET' CLASS IN RADAR LOCATION STATION AT EXPOSURE OF RATE INTERFERENCE

机译:暴露率干扰下在雷达定位站中支持“带涡轮喷气飞机”类空中目标的方法

摘要

FIELD: radio engineering, communication.;SUBSTANCE: method consists in parallel maintenaning based on Kalman filtering the Doppler frequency samples (DF) caused by the signal reflections from the group airframes and the centroid DF samples caused by the signal reflections from the impeller blades of the first compressor stage of the low pressure group aircraft engines; identifying impacts or absence of the interference leading away by rate based on the calculation of the derivative difference modules between the DF estimates, caused by the signal reflections from the airframe of each group aircraft and the DF centroid, caused by the signal reflections from the impeller blades of the first compressor stage of the low pressure group aircraft engines; comparing the moduli of the DF derivative differences with a threshold; when they do not exceed the threshold that corresponds to the exposure absence of the interferences leading away by rate, the DF estimates are formed in the output, calculated in accordance with the Kalman filtering procedure on the basis of observations, otherwise a decision is made about the exposure of the interferences leading away by rate and in the outputs along with the DF estimates, which are not identified as the interferences leading away by rate, the DF estimates are formed calculated on the basis of the reciprocal movement model of the radar carrier and that group aircraft, the reflected signal from which has not yet been identified initially as the interferences leading away by rate.;EFFECT: increasedf reliability of Doppler frequency estimates due to convergence rate of radar location station carrier with each group aircraft upon exposure of rate interference.;2 dwg
机译:领域:无线电工程,通信。实质:该方法包括基于Kalman滤波的并行维护,该滤波是由机组机身信号反射引起的多普勒频率样本(DF)和由叶轮叶片的信号反射引起的质心DF样本组成的。低压组合飞机发动机的第一级压缩机;基于DF估计值之间的导数差异模块的计算来确定速率导致的干扰的影响或不存在,该估计值是由每架飞机的机身和DF质心产生的信号反射所引起的,这些反射是由叶轮的信号反射引起的低压组飞机发动机的第一压缩机级的叶片;将DF导数差的模量与阈值进行比较;当它们不超过对应于因速率导致的无干扰暴露的阈值时,将在输出中形成DF估计值,并根据观测值根据Kalman滤波程序进行计算,否则就DF估计是在雷达载波的往复运动模型的基础上计算得出的,DF估计值和输出中的DF估计值(未确定为DF估计值的干扰)不相同。效果:由于雷达定位电台与每架飞机在速率干扰暴露后的收敛速度,多普勒频率估计的可靠性提高了。; 2 dwg

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