Preliminary Development and Flight Trials of a Cruise Altitude and Speed Optimization Decision Support Tool
Name
ICAT-2018-08_Clement Li_Report.pdf
Size
6.77 MB
Format
Adobe PDF
Checksum (MD5)
724bc07a5387fca938140f9e2643386e
Author(s)
Li, Clement
Hansman, R. John
Date Issued
October 11, 2018
Series/Report no.
;ICAT-2018-08
Abstract
A cruise altitude and speed optimization decision support tool, based on the concept of a minimum cost altitude tunnel, was developed to aid flight crew and dispatcher
situational awareness and decision-making in vertical trajectory planning in order to
reduce fuel and time costs. As the optimal altitude for an aircraft changes with speed,
weight, outside air temperature, and winds, flight crew decision-making can benefit
from the calculation and display of the relative flight costs of possible trajectories.
The concept of a minimum cost tunnel is introduced, and the decision support tool is
presented. Four preliminary flight trials were conducted with a Boeing 777-200 and
prototype decision support tool. The preliminary flight trials suggest that the decision
support tool is useful and improves situational awareness and coordination between
dispatcher and flight crew. The initial flight trials also indicated that flight crews
would benefit from higher quality turbulence information, including synchronization
of the turbulence information available to flight crews and dispatchers. The largest
fuel savings observed for a flight from the preliminary flight trials was over 3800 lbs.
Additionally, the flight trials suggest that the minimum cost tunnel would even be
useful as a static image included as part of the flight plan to provide situational
awareness and facilitate coordination with dispatchers.
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