• DocumentCode
    3201820
  • Title

    Stabilizing an S-band antenna for mobile communication from the moon

  • Author

    Desnoyer, Mark ; Guerin, Kelleher

  • Author_Institution
    Robot. Inst., Carnegie Mellon Univ., Pittsburgh, PA
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    The Google Lunar X-prize is a race for the first commercial program to fly a rover to the Moon and return imagery. In order to meet media expectations and generate significant revenue, this imagery must be in 720 p high definition format, which necessitates very high bandwidth communications. In order to provide such bandwidth throughout the mission, a high gain antenna must remain pointed at Earth, even while roving. This paper describes the simulation and performance analysis of a system to stabilize an S-band antenna for a moving X-prize class rover. To determine the necessary flight components and control system complexity, various sensor configurations are compared. These sensors include an Earth tracking camera, an inertial measurement unit and motor encoders. The resulting system demonstrates the pointing capability necessary to achieve a sustained 2.0 Mbps data transfer to a 13 m ground receiving dish, enough for a successful commercial venture to the Moon.
  • Keywords
    Moon; UHF antennas; aerospace instrumentation; microwave antennas; mobile communication; planetary rovers; space communication links; Earth tracking camera; Google Lunar X-prize; Moon; S-band antenna; flight components; flight control system complexity; inertial measurement; mobile communication; motor encoders; planetary rover; return imagery; Analytical models; Bandwidth; Cameras; Control systems; Earth; Mobile antennas; Mobile communication; Moon; Performance analysis; Sensor systems;
  • 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.2009.4839368
  • Filename
    4839368