Latest revision as of 22:52, 28 January 2021

Abstract

ources including wind prediction errors, pilot intent, surveillance errors, navigation errors and aircraft weight. The purpose of this study is to parametrically analyze the eects of aircraft speed errors on conflict detection and to analyze the performance of a conflict resolution algorithm when these speed errors are present. Results show that a speed error of 10% of the cruise speed can result in about 30% of the conflicts not being detected ten minutes before the loss of separation. It can also result in 50% more resolutions being performed to maintain separation.

Original document

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

• http://www.aviationsystemsdivision.arc.nasa.gov/publications/2010/Lauderdale_ATIO2010_Final.pdf

• http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9010,

http://dx.doi.org/10.2514/6.2010-9010

• https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110008377.pdf,

https://ntrs.nasa.gov/search.jsp?R=20110008377,

https://core.ac.uk/display/103785139,

https://trid.trb.org/view.aspx?id=1122895,

https://arc.aiaa.org/doi/10.2514/6.2010-9010,

https://repository.exst.jaxa.jp/dspace/handle/a-is/248018,

https://academic.microsoft.com/#/detail/1966076666