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Interval Management Systems Avionics Configuration Experiment (IMSACE) This study investigated the relative acceptance of different avionics implementations that present Flightdeck Interval Management (FIM) speeds and speed deviations to commercial pilots, and for indications of conditions that require action. Each crew evaluated four Avionics conditions: (1) Integrated in which the FIM target speed was presented in the upper left corner of the primary flight display (PFD) and speed profile deviation information was implicitly indicated as the deviation between current speed and an instantaneous speed profile bug on the PFD speed tape. In this Avionics condition, clearance information would have been entered, and could be referenced, on the FIM page in the MCDU. This page also gave a digital readout of speed profile deviation. Significant deviations from the speed profile triggered a message on the EICAS system. (2) EFB-Aft in which an aft-mounted EFB was used as the device housing the FIM algorithm and presented all the relevant information for the operation, including speed targets, speed deviation information, and all elements of the IM clearance. Significant deviations from the speed profile triggered messages on the same EFB display. (3) EFB-Fore in which the same information was presented as in the EFB-Aft condition, but the display was mounted in a more forward location, just under the outboard window. (4) EFB-Aft-AGD in which the EFB-Aft condition was augmented with the ADS-B Guidance Display (AGD). The AGD repeats the same FIM target speed and speed deviation information provided on the EFB. This study compares the efficacy of these Avionics Conditions as well as three methods of annunciating FIM events (a new speed, a reminder that a new speed occurred, and a deviation from the FIM speed profile), using only visual indications, visual indications and an aural for all events, or visual indications for all events plus an aural for speed deviations only. Results show clear preference for the Integrated condition and the use of aural indications. Other metrics of performance using these conditions and methods are mixed.
Document ID
20200007451
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Kara Latorella
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 14, 2020
Subject Category
Aeronautics (General)
Report/Patent Number
NF1676L-18030
Report Number: NF1676L-18030
Meeting Information
Meeting: Interval Management Systems Avionics Configuration Experiment (IMSACE) FAA Briefing
Location: Washington, DC
Country: US
Start Date: January 30, 2014
End Date: January 31, 2014
Sponsors: Federal Aviation Administration
Funding Number(s)
WBS: 031102.02.07.05.9D76.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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