Algorithms for aircraft track optimization in flexible routing

The authors consider the problem of optimization of aircraft flight tracks in air traffic management (ATM) on basis of flexible routing technologies which involve the use of satellite navigation systems (SNS). It is shown that in optimizing a trajectory it is necessary to take into account the accur...

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Main Authors: Skrypnik Oleg N., Netchaev Evgenii E., Arefyeva Natalya G., Arefyev Roman O.
Format: Article
Language:English
Published: EDP Sciences 2019-01-01
Series:ITM Web of Conferences
Online Access:https://www.itm-conferences.org/articles/itmconf/pdf/2019/07/itmconf_crimico2019_03003.pdf
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spelling doaj-44227b2fbd1742529ecac63b95e2be782021-03-02T09:31:35ZengEDP SciencesITM Web of Conferences2271-20972019-01-01300300310.1051/itmconf/20193003003itmconf_crimico2019_03003Algorithms for aircraft track optimization in flexible routingSkrypnik Oleg N.Netchaev Evgenii E.0Arefyeva Natalya G.1Arefyev Roman O.2Moscow State Technical University of Civil AviationIrkutsk Branch of Moscow State Technical University of Civil AviationIrkutsk Branch of Moscow State Technical University of Civil AviationThe authors consider the problem of optimization of aircraft flight tracks in air traffic management (ATM) on basis of flexible routing technologies which involve the use of satellite navigation systems (SNS). It is shown that in optimizing a trajectory it is necessary to take into account the accuracy of track holding in flight which depends on accuracy of the navigation system and external flight path disturbances, e.g. wind. For solving the problem of optimization the authors propose to use the theory of graphs. The technique of constructing a dynamic SNS accuracy field and representing it as a graph was developed. It is proposed that the SNS field could be characterized by geometric dilution of precision changing both in space and in time. Based on the theory of graphs (A-star algorithm) the technique of constructing a trajectory of optimal length under conditions of SNS accuracy variations and external flight path disturbances is proposed. The criterion of optimization based on minimizing the true track is offered. The cost function taking into account the track holding accuracy in navigating by SNS and effects of external flight disturbances is justified. The article represents the results of A-star algorithm application for optimal flight track construction under conditions of SNS accuracy field variation and presence of prohibited zones in the provide zone of airspacehttps://www.itm-conferences.org/articles/itmconf/pdf/2019/07/itmconf_crimico2019_03003.pdf
collection DOAJ
language English
format Article
sources DOAJ
author Skrypnik Oleg N.
Netchaev Evgenii E.
Arefyeva Natalya G.
Arefyev Roman O.
spellingShingle Skrypnik Oleg N.
Netchaev Evgenii E.
Arefyeva Natalya G.
Arefyev Roman O.
Algorithms for aircraft track optimization in flexible routing
ITM Web of Conferences
author_facet Skrypnik Oleg N.
Netchaev Evgenii E.
Arefyeva Natalya G.
Arefyev Roman O.
author_sort Skrypnik Oleg N.
title Algorithms for aircraft track optimization in flexible routing
title_short Algorithms for aircraft track optimization in flexible routing
title_full Algorithms for aircraft track optimization in flexible routing
title_fullStr Algorithms for aircraft track optimization in flexible routing
title_full_unstemmed Algorithms for aircraft track optimization in flexible routing
title_sort algorithms for aircraft track optimization in flexible routing
publisher EDP Sciences
series ITM Web of Conferences
issn 2271-2097
publishDate 2019-01-01
description The authors consider the problem of optimization of aircraft flight tracks in air traffic management (ATM) on basis of flexible routing technologies which involve the use of satellite navigation systems (SNS). It is shown that in optimizing a trajectory it is necessary to take into account the accuracy of track holding in flight which depends on accuracy of the navigation system and external flight path disturbances, e.g. wind. For solving the problem of optimization the authors propose to use the theory of graphs. The technique of constructing a dynamic SNS accuracy field and representing it as a graph was developed. It is proposed that the SNS field could be characterized by geometric dilution of precision changing both in space and in time. Based on the theory of graphs (A-star algorithm) the technique of constructing a trajectory of optimal length under conditions of SNS accuracy variations and external flight path disturbances is proposed. The criterion of optimization based on minimizing the true track is offered. The cost function taking into account the track holding accuracy in navigating by SNS and effects of external flight disturbances is justified. The article represents the results of A-star algorithm application for optimal flight track construction under conditions of SNS accuracy field variation and presence of prohibited zones in the provide zone of airspace
url https://www.itm-conferences.org/articles/itmconf/pdf/2019/07/itmconf_crimico2019_03003.pdf
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