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Operator Performance Evaluation of Fault Management Interfaces for Next-Generation SpacecraftIn the cockpit of the NASA's next generation of spacecraft, most of vehicle commanding will be carried out via electronic interfaces instead of hard cockpit switches. Checklists will be also displayed and completed on electronic procedure viewers rather than from paper. Transitioning to electronic cockpit interfaces opens up opportunities for more automated assistance, including automated root-cause diagnosis capability. The paper reports an empirical study evaluating two potential concepts for fault management interfaces incorporating two different levels of automation. The operator performance benefits produced by automation were assessed. Also, some design recommendations for spacecraft fault management interfaces are discussed.
Document ID
20090002609
Acquisition Source
Ames Research Center
Document Type
Contractor or Grantee Report
Authors
Hayashi, Miwa
(San Jose State Univ. Moffett Field, CA, United States)
Ravinder, Ujwala
(San Jose State Univ. Moffett Field, CA, United States)
Beutter, Brent
(NASA Ames Research Center Moffett Field, CA, United States)
McCann, Robert S.
(NASA Ames Research Center Moffett Field, CA, United States)
Spirkovska, Lilly
(NASA Ames Research Center Moffett Field, CA, United States)
Renema, Fritz
(Perot Systems Government Services United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
08ICES-0207
Funding Number(s)
CONTRACT_GRANT: NNX07AM07A
Distribution Limits
Public
Copyright
Other

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