• DocumentCode
    3202449
  • Title

    An antenna selection algorithm for Mars Exploration Rover to increase data return with minimum delay

  • Author

    Prathaban, Mahendiran ; Simu, Elena ; Kohlenberg, Josephine

  • Author_Institution
    IT/ Telecom Et Manage. SudParis, Evry
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    This paper proposes an antenna selection algorithm for Mars Exploration Rover (MER), where MER can autonomously select which antenna to use between X-band direct-to-Earth (DTE) and UHF for communication according to its constrains and limitation to effectively use their resources and thereby increase data return. When MER selects a path for communication, it simultaneously selects an antenna for transmission of data to earth. In our algorithm, we have defined a cost function for each possible path based on three parameters namely power required by the rover to transmit in that path, average delay, and error rate. A weighting is given to each parameter in the function based upon application quality of service (QoS) requirement. The algorithm has low computational complexity and provides optimum performance. This proposed algorithm would make MER more autonomous in terms of communication system. We have presented simulation results and analysis.
  • Keywords
    aerospace instrumentation; computational complexity; data communication; microwave antennas; planetary rovers; quality of service; space communication links; Mars Exploration Rover; X-band direct-to-Earth; antenna selection algorithm; computational complexity; data return; data transmission; minimum delay; quality of service; space communication; Computational complexity; Computational modeling; Cost function; Delay; Earth; Error analysis; Mars; Quality of service; Transmitting antennas; UHF antennas;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839398
  • Filename
    4839398