• DocumentCode
    447452
  • Title

    MER: from landing to six wheels on Mars...twice

  • Author

    Krajewski, Joel ; Burke, Kevin ; Lewicki, Chris ; Limonadi, Daniel ; Trebi-Ollennu, Ashitey ; Voorhees, Chris

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    2005
  • fDate
    10-12 Oct. 2005
  • Firstpage
    1791
  • Abstract
    Application of the pathfinder landing system design to enclose the much larger Mars Exploration Rover required a variety of rover deployments to achieve the surface driving configuration. The project schedule demanded that software, design, engineering model test, and flight hardware build be accomplished in parallel. This challenge was met through (a) bounding unknown environments against which to design and test, (b) early mechanical prototype testing, (c) constraining the scope of on-board autonomy to survival-critical deployments, (d) executing a balance of nominal and off-nominal test cases, (e) developing off-nominal event mitigation techniques before landing, (f) flexible replanning in response to surprises during operations. Here is discussed several specific events encountered during initial MER surface operations.
  • Keywords
    Mars; aircraft landing guidance; planetary rovers; Mars Exploration Rover; event mitigation technique; mechanical prototype testing; pathfinder landing system design; rover deployment; spacecraft mechanism; surface driving configuration; surface operation; Aerospace engineering; Application software; Design engineering; Hardware; Mars; Prototypes; Software design; Software prototyping; Software testing; Wheels; Airbags; Egress; ITE; MER; Rover Deployments; Spacecraft Mechanisms; Standup; Surface Operations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems, Man and Cybernetics, 2005 IEEE International Conference on
  • Print_ISBN
    0-7803-9298-1
  • Type

    conf

  • DOI
    10.1109/ICSMC.2005.1571408
  • Filename
    1571408