DocumentCode
2534245
Title
Airborne 4-dimensional trajectory management
Author
Honzik, B. ; Herodes, M.
Author_Institution
Honeywell, Adv. Technol. Eur., Brno, Czech Republic
fYear
2012
fDate
14-18 Oct. 2012
Abstract
The paper describes a prototype of an airborne Flight Management System (FMS), supporting initial four-dimensional (I-4D) flight operations. The I-4D operations are based on airborne computed predictions that are used in ground systems. The goal is to establish far in advance a sequence for all aircraft converging to a merging point in a congested area. After coordination between the ground systems and aircraft, a time constraint at a merging point is assigned to each aircraft. As compensation, aircraft are allowed to fly their optimum profile up to that point, without any vectoring instructions from controllers. The prototype is based on Airbus A320 FMS software which has been enhanced by the I-4D features like Required Time of Arrival (RTA) in descent flight phase, reliable RTA window computation, and data link enhancements. Example of operational scenario is presented. The prototype has been tested with actual hardware, in an Airbus cockpit simulator and in flight as well.
Keywords
air traffic; ground support systems; time-of-arrival estimation; Airbus A320 FMS software; Airbus cockpit simulator; RTA; airborne 4D trajectory management; airborne FMS; aircraft ground system; data link enhancement; descent flight phase; flight management system; merging point; required time of arrival; Air traffic control; Aircraft; Meteorology; Prototypes; Reliability; Standards; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location
Williamsburg, VA
ISSN
2155-7195
Print_ISBN
978-1-4673-1699-6
Type
conf
DOI
10.1109/DASC.2012.6382317
Filename
6382317
Link To Document