首页> 外国专利> MEASUREMENT OF WAVE REFRACTIVE INDEX OF IONOSPHERE AND ATMOSPHERIC GAS LAYER VIA FOLLOW-UP OF WAVE PROPAGATION ROUTE AND MEASUREMENT OF RELATIVE POSITION BETWEEN TARGET AND OBSERVATION POINT

MEASUREMENT OF WAVE REFRACTIVE INDEX OF IONOSPHERE AND ATMOSPHERIC GAS LAYER VIA FOLLOW-UP OF WAVE PROPAGATION ROUTE AND MEASUREMENT OF RELATIVE POSITION BETWEEN TARGET AND OBSERVATION POINT

机译:通过波传播路径的跟踪和目标与观测点之间相对位置的测量来测量电离层和大气层的波折射指数

摘要

PURPOSE: To accurately measure the cosine of the critical incident angle of a wave to an ionosphere by following up the wave from the position of a satellite assumed on the basis of a wave propagation time therefrom and the approximate value of a vertical distance between horizontal planes across the satellite and an observation point on the ground. ;CONSTITUTION: The virtual point P1 of a satellite (point P) is set on the basis of the approximate value of the 3D position of the point P obtained from a wave transmitted from the satellite, and a linear distance between the point P1 and an observation point A on the ground is divided by a flux (u), thereby establishing a wave propagation time pi. Then, a virtual point P'1 is set on a wave propagation route P1CA with length P1DA kept equal to P'1CA, so that a wave from the point P1 can reach in the propagation time P1. Also, the virtual point P2 of the satellite is established, so as to keep route length P2EA equal to P'1CA, thereby obtaining a vertical distance Lzi. between horizontal planes across the point P2 and the observation point A. As a result, a critical incident angle αio when a wave passing the route P2EA enters the interface of a wave rectilinear propagation layer and an ionosphere, can be detected, thereby improving the measurement accuracy of the 3D position of the satellite.;COPYRIGHT: (C)1995,JPO
机译:目的:通过根据从卫星位置传来的波并根据其传播时间和水平面之间的垂直距离的近似值来跟踪该波,从而精确测量波与电离层临界入射角的余弦值穿过卫星和地面上的观察点。 ;构成:卫星的虚拟点P 1 (点P)是根据从卫星发射的波中获得的点P的3D位置的近似值和P 1 与地面观测点A之间的线性距离除以通量(u),从而确定波传播时间p i 。然后,在波传播路径P 1 CA上设置虚拟点P' 1 ,长度P 1 DA等于P'< Sub> 1 CA,以便从点P 1 发出的波可以在传播时间P 1 中到达。此外,建立卫星的虚拟点P 2 ,以使路由长度P 2 EA等于P' 1 CA,从而获得垂直距离L zi 。因此,当波通过路径P 2 <时,临界入射角α io 。 / Sub> EA进入波的直线传播层和电离层的界面,可以被检测到,从而提高了卫星3D位置的测量精度。;版权:(C)1995,JPO

著录项

  • 公开/公告号JPH07260918A

    专利类型

  • 公开/公告日1995-10-13

    原文格式PDF

  • 申请/专利权人 KAWAMATA KENICHI;

    申请/专利号JP19940079447

  • 发明设计人 KAWAMATA KENICHI;

    申请日1994-03-26

  • 分类号G01S5/02;G01N22/00;

  • 国家 JP

  • 入库时间 2022-08-22 04:29:46

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