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A Cognitive Engineering Analysis of the Vertical Navigation (VNAV) FunctionA cognitive engineering analysis of the Flight Management System (FMS) Vertical Navigation (VNAV) function has identified overloading of the VNAV button and overloading of the Flight Mode Annunciator (FMA) used by the VNAV function. These two types of overloading, resulting in modal input devices and ambiguous feedback, are well known sources of operator confusion, and explain, in part, the operational issues experienced by airline pilots using VNAV in descent and approach. A proposal to modify the existing VNAV design to eliminate the overloading is discussed. The proposed design improves pilot's situational awareness of the VNAV function, and potentially reduces the cost of software development and improves safety.
Document ID
20010046486
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Sherry, Lance
(RAND/Honeywell International, Inc. Phoenix, AZ United States)
Feary, Michael
(NASA Ames Research Center Moffett Field, CA United States)
Polson, Peter
(Colorado Univ. Boulder, CO United States)
Mumaw, Randall
(Boeing Computer Services Co. Seattle, WA United States)
Palmer, Everett
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2001
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NAS 1.15:210915
NASA/TM-2001-210915
Funding Number(s)
PROJECT: RTOP 711-41-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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