• DocumentCode
    1409445
  • Title

    Use of satellites for navigation

  • Author

    Chu, Juo-Wen

  • Author_Institution
    Aeronautics Navigation Services and Maintenance Office, CAA, Taipei, Taiwan, Republic of China
  • Issue
    5
  • fYear
    1968
  • Firstpage
    799
  • Lastpage
    800
  • Abstract
    Any position on earth can be determined as the intersection of two circles, with their centers located at 0 and 0´ on the earth´s surface just beneath two satellites. Therefore any flying path can be described as a locus of many such positions. One synchronous satellite can cover 45 percent of the surface of the earth. When an aircraft flies outbound along the earth´s surface from the reference point 0, the traveling time of the wave pulses transmitted from the satellite to the aircraft becomes longer and longer, but it is not proportional to the flying distance, because the altitude angle (the intersection angle between the line from the satellite to the measured point and the tangent line to the earth´s surface at the point) changes from time to time. The increase of the transit time will be less when flying the same distance over the area near the reference point than it would be farther away. A correction factor cos(90-α-β) should be introduced to equalize the measured distance to the true flying distance.
  • Keywords
    Earth; Frequency synchronization; Position measurement; Pulse generation; Pulse measurements; Satellite navigation systems;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1968.5408698
  • Filename
    5408698