Methodology for collision risk assessment of an airspace flow corridor concept

This paper presents a methodology to estimate the collision risk associated with a future air-transportation concept called the flow corridor. This concept is designed to reduce congestion and increase throughput in en-route airspace by creating dedicated flight corridors across the continent. The m...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Reliability engineering & system safety 2015-10, Vol.142, p.444-455
Hauptverfasser: Zhang, Yimin, Shortle, John, Sherry, Lance
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:This paper presents a methodology to estimate the collision risk associated with a future air-transportation concept called the flow corridor. This concept is designed to reduce congestion and increase throughput in en-route airspace by creating dedicated flight corridors across the continent. The methodology is a hybrid collision-risk methodology combining Monte Carlo simulation and dynamic event trees. Monte Carlo simulation is used to model the movement of aircraft within the corridor and to identify potential trajectories that might lead to a collision. Dynamic event trees are used to evaluate the effectiveness of subsequent safety layers that protect against collisions. The overall risk assessment captures the unique characteristics of the flow corridor concept, including self-separation within the corridor, lane change maneuvers, speed adjustments, and the automated separation assurance system. A tradeoff between safety and throughput is conducted, and a sensitivity analysis identifies the most critical parameters in the model. •A methodology is developed to estimate the collision risk of flow corridor concept.•Unique characteristics of the flow corridor concept are included.•The flow corridor concept can meet an international target level of safety.•Throughput can be increased by reducing separation to 2 nautical miles.
ISSN:0951-8320
1879-0836
DOI:10.1016/j.ress.2015.05.015