NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Understanding Extended Projected Profile (EPP) Trajectory Error Using a Medium-Fidelity Aircraft SimulationA critical component of Trajectory-Based Operations is the ability for a consistent and accurate 4-dimensional trajectory to be shared and synchronized between airborne and ground systems as well as amongst various ground automation systems. The Aeronautical Telecommunication Network—Baseline 2 standard defines the Extended Projected Profile (EPP) trajectory that can be sent via Automatic Dependent Surveillance-Contract from an aircraft to ground automation. The EPP trajectory message contains a representation of the reference trajectory from an aircraft’s Flight Management System (FMS). In this work, a set of scenarios were run in a medium-fidelity aircraft and FMS simulation to perform an initial characterization of EPP trajectory errors under a given set of conditions. The parameters investigated were the route length, route type, wind magnitude error, wind direction error, and with and without a required time-of-arrival constraint.




Document ID
20200002313
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Guerreiro, Nelson M.
(NASA Langley Research Center Hampton, VA, United States)
Underwood, Matthew C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 13, 2020
Publication Date
June 25, 2018
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-28648
Meeting Information
Meeting: AIAA Aviation 2018 and Aeronautics Forum and Exposition (AIAA AVIATION 2018)
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 28, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 629660.03.10.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available