Evaluation of Flight Deck-Based Interval Management Crew Procedure FeasibilityAir traffic demand is predicted to increase over the next 20 years, creating a need for new technologies and procedures to support this growth in a safe and efficient manner. The National Aeronautics and Space Administration's (NASA) Air Traffic Management Technology Demonstration - 1 (ATD-1) will operationally demonstrate the feasibility of efficient arrival operations combining ground-based and airborne NASA technologies. The integration of these technologies will increase throughput, reduce delay, conserve fuel, and minimize environmental impacts. The ground-based tools include Traffic Management Advisor with Terminal Metering for precise time-based scheduling and Controller Managed Spacing decision support tools for better managing aircraft delay with speed control. The core airborne technology in ATD-1 is Flight deck-based Interval Management (FIM). FIM tools provide pilots with speed commands calculated using information from Automatic Dependent Surveillance - Broadcast. The precise merging and spacing enabled by FIM avionics and flight crew procedures will reduce excess spacing buffers and result in higher terminal throughput. This paper describes a human-in-the-loop experiment designed to assess the acceptability and feasibility of the ATD-1 procedures used in a voice communications environment. This experiment utilized the ATD-1 integrated system of ground-based and airborne technologies. Pilot participants flew a high-fidelity fixed base simulator equipped with an airborne spacing algorithm and a FIM crew interface. Experiment scenarios involved multiple air traffic flows into the Dallas-Fort Worth Terminal Radar Control airspace. Results indicate that the proposed procedures were feasible for use by flight crews in a voice communications environment. The delivery accuracy at the achieve-by point was within +/- five seconds and the delivery precision was less than five seconds. Furthermore, FIM speed commands occurred at a rate of less than one per minute, and pilots found the frequency of the speed commands to be acceptable at all times throughout the experiment scenarios.
Document ID
20140002409
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wilson, Sara R. (NASA Langley Research Center Hampton, VA, United States)
Murdoch, Jennifer L. (NASA Langley Research Center Hampton, VA, United States)
Hubbs, Clay E. (National Inst. of Aerospace Hampton, VA, United States)
Swieringa, Kurt A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 28, 2014
Publication Date
August 19, 2013
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-16028Report Number: NF1676L-16028
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference
Location: Boston, MA
Country: United States
Start Date: August 19, 2013
End Date: August 22, 2013
Sponsors: American Inst. of Aeronautics and Astronautics