DocumentCode
1751378
Title
Stability and performance of intersecting aircraft flows under sequential conflict resolution
Author
Mao, Zhi-Hong ; Feron, Eric
Author_Institution
Dept. of Aeronaut. & Astronaut., MIT, Cambridge, MA, USA
Volume
2
fYear
2001
fDate
2001
Firstpage
722
Abstract
This paper considers the problem of intersecting aircraft flows under sequential conflict avoidance rules. Using an Eulerian standpoint (aircraft flow through a fixed control volume), new air traffic control models and scenarios are defined that enable the study of long-term airspace stability problems. As a generalization to the basic aircraft flow model discussed previously, this paper considers conflict scenarios involving arbitrary encounter angles, different times to conflict, and different aircraft flow speeds. It is shown that airspace stability, defined both in terms of safety and performance, is preserved under sequential conflict resolution algorithms. Performance bounds are derived for the aircraft flow problem. For more than two intersecting aircraft flows, simulations indicate that flow stability may not be guaranteed under simple sequential conflict avoidance rules
Keywords
aerospace simulation; air traffic control; stability; Eulerian standpoint; air traffic control models; airspace stability; intersecting aircraft flows; performance evaluation; sequential conflict avoidance rules; sequential conflict resolution; stability; Aerospace control; Air safety; Air traffic control; Air transportation; Aircraft manufacture; Aircraft navigation; Centralized control; Space technology; Stability; Traffic control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.945800
Filename
945800
Link To Document