The 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.
Takeoff Performance Monitoring System display options
AIAA/AHS Flight Simulation Technologies Conference ; 1992 ; Hilton Head Island, SC, United States
01.01.1992
Aufsatz (Konferenz)
Keine Angabe
Englisch
Takeoff Performance Monitoring System Display Options
Online Contents | 1994
|Takeoff Performance Monitoring System display options
AIAA | 1992
|Takeoff performance monitoring system display options
AIAA | 1994
|