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

Content Provider	IEEE Xplore Digital Library
Author	Marquez, J.J. Ramirez, M.
Copyright Year	2014
Description	Author affiliation: NASA Ames Res. Center, San Jose State Univ., Moffett Field, IA, USA (Ramirez, M.) \|\| NASA Ames Res. Center, Moffett Field, IA, USA (Marquez, J.J.)
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.
Sponsorship	IEEE Aerosp. Electron. Syst. Soc.
Starting Page	1
Ending Page	10
File Size	1478545
Page Count	10
File Format	PDF
e-ISBN	9781479916221
DOI	10.1109/AERO.2014.6836314
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-03-01
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Automation Training Moon Radar Space vehicles Monitoring
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

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

Small lunar lander/hopper performance analysis

Performance evaluation of radio frequency of Cassini Radar

Feasibility and design of the surface penetrating radar for lunar lander

Small lunar lander/hopper navigation analysis using linear covariance

Descent Assisted Split Habitat Lunar Lander Concept

Apollo manned spacecraft antenna systems for the lunar mission

Effects of an achievability display during simulated lunar landings

Lunar Surface Propagation Modeling and Effects on Communications

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

Similar Documents

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

Small lunar lander/hopper performance analysis

Performance evaluation of radio frequency of Cassini Radar

Feasibility and design of the surface penetrating radar for lunar lander

Small lunar lander/hopper navigation analysis using linear covariance

Descent Assisted Split Habitat Lunar Lander Concept

Apollo manned spacecraft antenna systems for the lunar mission

Effects of an achievability display during simulated lunar landings

Lunar Surface Propagation Modeling and Effects on Communications

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