• DocumentCode
    158273
  • Title

    Level of automation and failure frequency effects on simulated lunar lander performance

  • Author

    Marquez, Jessica J. ; Ramirez, M.

  • Author_Institution
    NASA Ames Res. Center, Moffett Field, IA, USA
  • fYear
    2014
  • fDate
    1-8 March 2014
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    A human-in-the-loop experiment was conducted at the NASA Ames Research Center Vertical Motion Simulator, where instrument-rated pilots completed a simulated terminal descent phase of a lunar landing. Ten pilots participated in a 2 x 2 mixed design experiment, with level of automation as the within-subjects factor and failure frequency as the between-subjects factor. The two evaluated levels of automation were high (fully automated landing) and low (manual controlled landing). During test trials, participants were exposed to either a high number of failures (75% failure frequency) or low number of failures (25% failure frequency). In order to investigate the pilots´ sensitivity to changes in levels of automation and failure frequency, the dependent measure selected for this experiment was accuracy of failure diagnosis, from which D Prime and Decision Criterion were derived. For each of the dependent measures, no significant difference was found for level of automation and no significant interaction was detected between level of automation and failure frequency. A significant effect was identified for failure frequency suggesting failure frequency has a significant effect on pilots´ sensitivity to failure detection and diagnosis. Participants were more likely to correctly identify and diagnose failures if they experienced the higher levels of failures, regardless of level of automation.
  • Keywords
    decision theory; entry, descent and landing (spacecraft); failure analysis; fault diagnosis; planetary rovers; D prime; automation level effect; decision criterion; failure detection; failure diagnosis; failure frequency effect; human-in-the-loop experiment; pilot sensitivity; simulated lunar landing performance; simulated terminal descent phase; Automation; Monitoring; Moon; Radar; Space vehicles; Training;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2014 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5582-4
  • Type

    conf

  • DOI
    10.1109/AERO.2014.6836314
  • Filename
    6836314