Abstract

next-generation air traffic decision support tool, known as the active final approach spacing tool (aFAST), will generate heading, speed and altitude commands to achieve more precise separation of aircraft in the terminal area. The techniques used to analyze the performance of earlier generation decision support tools are not adequate to analyze the performance of aFAST. The paper summarizes the development of a new and innovative fully closed-loop testing method for aFAST. This method, called trajectory feedback testing, closes each aircraft control loop inside of the aFAST scheduling algorithm. Validation of trajectory feedback testing by examination of the variation of aircraft time-of-arrival predictions between schedule updates and the variation of aircraft excess separation distances between simulation runs is presented.


Original document

The different versions of the original document can be found in:

http://dx.doi.org/10.1109/acc.2002.1023204 under the license cc0
http://ieeexplore.ieee.org/xpl/freeabs_all.jsp?isnumber=22015&arnumber=1023204&count=152&index=84,
https://ieeexplore.ieee.org/xpl/freeabs_all.jsp?isnumber=22015&arnumber=1023204&count=152&index=84,
https://www.aviationsystems.arc.nasa.gov/publications/terminal/fast/robinson_05_02.pdf,
http://www.aviationsystemsdivision.arc.nasa.gov/publications/terminal/fast/robinson_05_02.pdf,
https://academic.microsoft.com/#/detail/2069045004
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Document information

Published on 01/01/2002

Volume 2002, 2002
DOI: 10.1109/acc.2002.1023204
Licence: Other

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