• DocumentCode
    1769754
  • Title

    GNSS software receiver as navigation sensor in very high orbits

  • Author

    Palmerini, G.B.

  • Author_Institution
    DIAEE - Dipt. di Ing. Astronautica, Elettr. ed Energetica, Sapienza Univ. di Roma, Rome, Italy
  • fYear
    2014
  • fDate
    29-30 May 2014
  • Firstpage
    34
  • Lastpage
    38
  • Abstract
    Space navigation in very high Earth orbits and in lunar transfers is based mainly on ground-based tracking. It can be possible to spare the expensive and complex control segment by making the most of Global Navigation Satellite Systems (GNSS). A suitable receiver would be an application-specific sensor, based on software radio architecture and quite different from typical terrestrial devices, meaning that it will lacks the tracking section and will work in the so-called snapshot mode. The knowledge of the orbital dynamics and a moderate quality onboard clock can provide a first solution estimate which is accurate enough for the sensor to meaningfully exploit, with the help of a limited external aiding, the received signals. The receiver therefore becomes a navigation sensor working outside the primary GNSS service volume, where signals are extremely weak and frequently disrupted by outages.
  • Keywords
    satellite navigation; software radio; GNSS software receiver; Global Navigation Satellite Systems; ground-based tracking; lunar transfers; moderate quality onboard clock; navigation sensor; orbital dynamics; primary GNSS service volume; software radio architecture; very high Earth orbits; Global Positioning System; Moon; Orbits; Receivers; Space vehicles; GNSS; navigation sensors; pseudorange measurements; software receiver; space navigation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
  • Conference_Location
    Benevento
  • Type

    conf

  • DOI
    10.1109/MetroAeroSpace.2014.6865890
  • Filename
    6865890