Safety performance functions to predict separation minima infringements in en-route airspace

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Abstract

Purpose: The purpose of this study is to establish a systematic framework to characterise the safety of air routes, in terms of separation minima infringements (SMIs) between en-route aircraft, based on the definition of models known as safety performance functions. Design/methodology/approach: Techniques with high predictive capability were selected that enable both expert knowledge and data to be harnessed: Bayesian networks. It was necessary to establish a conceptual framework that integrates the knowledge currently available on the causality and precursors of SMIs with the hindsight derived from the analysis of the type of data available. To translate the conceptual framework into a set of causal subnets, the concepts of air traffic management (ATM) barrier model and event trees have been incorporated. Findings: The model combines analytics and insights, as well as predictive capability, to answer the question of how airspace separation infringements are produced and what their frequency of occurrence will be. The main outputs of the network are the predicted probability of success for the ATM barriers and the predicted probability distribution of the vertical and horizontal separation of an aircraft in its closest point of approach. Originality/value: The main contribution of this work is that, by virtue of the calculation capacity obtained, the network can be used to draw conclusions about the impact that a modification of the airspace and of the traffic, or operational conditions, would have on the effectiveness of the barriers and on the final distributions of distance between aircraft in the CPA, thereby estimating the probability of SMI.

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APA

Delgado-Aguilera Jurado, R., Gómez Comendador, V. F., Zamarreño Suárez, M., Pérez Moreno, F., Verdonk Gallego, C. E., & Arnaldo Valdes, R. M. (2022). Safety performance functions to predict separation minima infringements in en-route airspace. Aircraft Engineering and Aerospace Technology, 94(9), 1546–1555. https://doi.org/10.1108/AEAT-11-2021-0331

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