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Takeoff Performance Monitoring System display optionsThe development of displays for the Takeoff Performance Monitoring System (TPMS) is described with attention given to the three concepts prepared for commercial applications. The TPMS algorithm is described and related to the display requirements for pilots of two-engine airplanes. Head-up and -down displays are considered for displaying the simple advisory data which indicate whether the takeoff is a 'Go' or 'No-go' based on engine failure, acceleration error, and runway length. Six pilots are shown the three display options which include: (1) basic information; (2) basic data with 'Go/No-go' advisory flags; and (3) basic data, advisory flags, and an abort-warning symbol. The pilots tended to select the option with the most advisory data available, but the inconclusive preference study led to the concept of presenting all three configurations as possible display options for the TPMS.
Document ID
19920069809
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Middleton, David B.
(NASA Langley Research Center Hampton, VA, United States)
Srivatsan, Raghavachari
(Vigyan, Inc. Hampton, VA, United States)
Person, Lee H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Instrumentation
Report/Patent Number
AIAA PAPER 92-4138
Meeting Information
Meeting: AIAA/AHS Flight Simulation Technologies Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AHS, AIAA
Accession Number
92A52433
Distribution Limits
Public
Copyright
Other

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