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Distance measurement method of satellite considering quantum and gravity effects, location measurement method using the same, and user terminal

机译:考虑量子和重力效应的卫星距离测量方法,使用相同的位置测量方法和用户终端

摘要

The method for measuring the distance of an artificial satellite according to an exemplary embodiment of the present invention comprises the steps of: receiving, by an electronic device, linearly polarized photons from the artificial satellite and angular momentum per unit mass of the artificial satellite; measuring a rotation amount of polarized light due to warping in space-time, and calculating, by an electronic device, a distance to the artificial satellite using the rotation amount of the polarized light and angular momentum per unit mass of the artificial satellite. In this case, in the step of calculating the distance to the artificial satellite using the rotation amount of the polarized light and the angular momentum per unit mass of the artificial satellite, the distance to the artificial satellite is obtained by the following relational expression, , (Where r is the distance to the satellite, 2Θ is the amount of rotation of polarized light, l obs is the angular momentum per unit mass of the satellite, and rs is the Schwarzschild radius of the Earth).
机译:根据本发明示例性实施例的用于测量人造卫星距离的方法包括以下步骤:通过电子器件接收来自人造卫星的线性偏振光子,每单位质量的人造卫星的角动量;通过在时空中的翘曲和通过电子设备计算到人造卫星的旋转量来测量由于在时空的翘曲和计算偏振的距离和每单位卫星的角动量来计算偏振光的旋转量。在这种情况下,在使用偏振光的旋转量和每单位卫星的每单位质量的角动量计算到人造卫星的步骤中,通过以下关系表达获得与人造卫星的距离, (其中R是卫星的距离,2θ是偏振光的旋转量,L OBS是每单位卫星的角动量,并且Rs是地球的Schwarzschild半径)。

著录项

  • 公开/公告号KR102362758B1

    专利类型

  • 公开/公告日2022-02-11

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR1020200096015

  • 发明设计人 안도열;

    申请日2020-07-31

  • 分类号G01S19/23;G01S19/20;G01S19/39;

  • 国家 KR

  • 入库时间 2022-08-24 23:38:09

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