首页> 外国专利> METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A SATELLITE IN THE TRANSFER PHASE FROM AN INITIAL ORBIT TO A MISSION ORBIT

METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A SATELLITE IN THE TRANSFER PHASE FROM AN INITIAL ORBIT TO A MISSION ORBIT

机译:估算从初始轨道到发射轨道的转移阶段中卫星方向的方法和系统

摘要

A method for estimating a direction of a satellite in the transfer phase. The direction of the satellite is estimated relative to a measurement antenna by executing steps for measuring the reception power, by the measurement antenna, of a target signal emitted by the satellite, for different pointing directions of the measurement antenna. The target signal has a substantially sinusoidal component referred to as a single-frequency component. Each power measurement step includes a transposition in the frequency domain of a digital signal, obtained from a signal supplied by the measurement antenna, to obtain a frequency spectrum of the digital signal over a predetermined frequency band having the single-frequency component. The power measurement for the pointing direction being considered is determined based on a maximum value of the frequency spectrum.
机译:一种在转移阶段估计卫星方向的方法。通过执行用于针对测量天线的不同指向方向执行用于通过测量天线测量由卫星发射的目标信号的接收功率的步骤,相对于测量天线来估计卫星的方向。目标信号具有被称为单频分量的基本上正弦的分量。每个功率测量步骤包括从由测量天线提供的信号获得的数字信号的频域中的换位,以在具有单频分量的预定频带上获得数字信号的频谱。基于频谱的最大值来确定所考虑的指向方向的功率测量。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号