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ASSESSMENT SYSTEM OF INTERFERENCE IMMUNITY OF NAVIGATION CIRCUIT OF ARTIFICIAL EARTH SATELLITE (AES)

机译:人造卫星(AES)导航电路干扰抗扰性评估系统

摘要

FIELD: radio engineering.;SUBSTANCE: assessment system of interference immunity of navigation circuit of artificial Earth satellite comprises simulator of trajectory measurements without action of radio interference, shaping unit of trajectory measurements disturbed with errors owing to the action of radio interference, simulator of errors owing to the action of radio interference, calculation unit of the ratio of signal power to radio interference power, input data unit, prediction unit of AES movement parameters, calculation unit of the measured parameter values, unit for determining the parameters of AES movement as per trajectory measurements without any action of radio interference, unit for determining the parameters of AES movement as per trajectory measurements, which are disturbed with errors due to radio interference action, and assessment unit of accuracy of determination of AES movement parameters under conditions of the action of radio interference which are related to each other in certain way.;EFFECT: obtaining the assessments of accuracy of determination of AES orbit parameters at the measuring interval for AES of any class under conditions of radio interference action.;1 dwg
机译:领域:无线电工程。;物质:人造地球卫星导航电路抗干扰性评估系统,包括没有无线电干扰作用的轨迹测量模拟器,由于无线电干扰的作用而被误差干扰的轨迹测量整形单元,误差模拟器由于无线电干扰的作用,信号功率与无线电干扰功率之比的计算单位,输入数据单位,AES运动参数的预测单位,实测参数值的计算单位,用于确定AES运动参数的单位在没有无线电干扰作用的情况下进行轨迹测量,根据轨迹测量确定AES运动参数的单元,该运动因无线电干扰作用而被误差所干扰,并且在运动条件下确定AES运动参数准确性的评估单元与EAC有关的无线电干扰效果:在无线电干扰作用条件下,在任何等级的AES的测量间隔内,获得确定AES轨道参数的准确性评估; 1 dwg

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