Scipediacontent: Scipediacontent moved page Draft Content 708175027 to Hand et al 2010a

2021-02-01T23:58:55Z

Scipediacontent moved page Draft Content 708175027 to Hand et al 2010a

Scipediacontent: Created page with " == Abstract == This paper discusses the effect of sequential conflict resolution maneuvers of an infinite aircraft flow through a finite control volume. Aircraft flow models..."

2021-02-01T23:58:50Z

Created page with " == Abstract == This paper discusses the effect of sequential conflict resolution maneuvers of an infinite aircraft flow through a finite control volume. Aircraft flow models..."

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== Abstract ==

This paper discusses the effect of sequential conflict resolution maneuvers of an infinite aircraft flow through a finite control volume. Aircraft flow models are utilized to simulate traffic flows and determine stability. Pseudo-random flow geometry is considered to determine airspace stability in a more random airspace, where aircraft flows are spread over a given positive width. The use of this aircraft flow model generates a more realistic flow geometry. A set of upper bounds on the maximal aircraft deviation during conflict resolution is derived. Also with this flow geometry it is proven that these bounds are not symmetric, unlike the symmetric bounds derived in previous papers for simpler flow configurations. Stability is preserved under sequential conflict resolution algorithms for all flow geometries discussed in this paper.

Comment: 6 pages, 8 figures, ACC 2011 initial submission(5 pages 8 figures for ieeeconf style)

== Original document ==

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

* [http://arxiv.org/abs/1010.0448 http://arxiv.org/abs/1010.0448]

* [http://arxiv.org/pdf/1010.0448.pdf http://arxiv.org/pdf/1010.0448.pdf]

* [http://www.nt.ntnu.no/users/skoge/prost/proceedings/acc11/data/papers/1285.pdf http://www.nt.ntnu.no/users/skoge/prost/proceedings/acc11/data/papers/1285.pdf],
: [http://yadda.icm.edu.pl/yadda/element/bwmeta1.element.ieee-000005991516 http://yadda.icm.edu.pl/yadda/element/bwmeta1.element.ieee-000005991516],
: [http://ui.adsabs.harvard.edu/abs/2010arXiv1010.0448H/abstract http://ui.adsabs.harvard.edu/abs/2010arXiv1010.0448H/abstract],
: [https://ieeexplore.ieee.org/document/5991516 https://ieeexplore.ieee.org/document/5991516],
: [http://ieeexplore.ieee.org/document/5991516 http://ieeexplore.ieee.org/document/5991516],
: [https://academic.microsoft.com/#/detail/2128856506 https://academic.microsoft.com/#/detail/2128856506]

* [http://xplorestaging.ieee.org/ielx5/5975310/5989965/05991516.pdf?arnumber=5991516 http://xplorestaging.ieee.org/ielx5/5975310/5989965/05991516.pdf?arnumber=5991516],
: [http://dx.doi.org/10.1109/acc.2011.5991516 http://dx.doi.org/10.1109/acc.2011.5991516]

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Hand et al 2010a - Revision history

Scipediacontent: Scipediacontent moved page Draft Content 708175027 to Hand et al 2010a

Scipediacontent: Created page with " == Abstract == This paper discusses the effect of sequential conflict resolution maneuvers of an infinite aircraft flow through a finite control volume. Aircraft flow models..."