• DocumentCode
    3509764
  • Title

    Axel Mobility Platform for Steep Terrain Excursions and Sampling on Planetary Surfaces

  • Author

    Nesnas, Issa A D ; Abad-Manterola, Pablo ; Edlund, Jeffrey A. ; Burdick, Joel W.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    11
  • Abstract
    The recent discovery of bright new deposits in two crater gullies on Mars suggests that water still flows in brief spurts on Mars. In this paper, we will present the Axel rover (Figure 1) that was developed to access and sample such deposits on the inside of steep crater walls. Axel is a tethered rover that can be a payload on a lander or a larger rover. The primary features of Axel are its minimal complexity and robustness to the treacherous terrain of sites that are of scientific interest. Using a symmetrical design with three actuators, Axel is capable of operating upside down and right side up, enabling it to descend over crater promontories. With its actuated trailing link, Axel can operate on both flat and sloped terrains. Using a sampling device mounted on the trailing link, Axel can collect and store terrain samples and return to its host platform for detailed scientific sample analysis. We will present our preliminary results that demonstrated Axel´s ability to traverse both flat and sloped rocky terrain including 90deg vertical cliffs and collecting soil samples on slopes ranging from 10deg - 40deg in the JPL Mars Yard.
  • Keywords
    planetary rovers; axel mobility platform; planetary surfaces; steep terrain excursions; tethered rover; Actuators; Laboratories; Mars; Payloads; Propulsion; Prototypes; Robots; Robustness; Sampling methods; Soil;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526235
  • Filename
    4526235