Abstract:An air traffic control system's main function is to separate aircraft. The computer supporting the system assists the air traffic controllers by generating a conflict alert whenever it predicts that two aircraft are about to get too close to each other. The performance of the conflict alert function is a key element to the overall functioning of the air traffic control system. A set of metrics has been designed to measure the conflict alerting performance of an aircraft traffic control system. The key factors … Show more
“…This approach relies on the use of a linear predictor operating on truth data to check the validity and timeliness of an alert. A similar approach is described in [7] and [8], using however smooth and interpolated track outputs instead of truth data.…”
Section: Introductionmentioning
confidence: 91%
“…For 3 The term "valid-late" has also been applied to such alerts [8] instance, ERAM had requirements to be able to perform surveillance processing over an area as large as 2000 nmi by 2000 nmi with a specified mix of short and long range radars providing multiple radar coverage in some areas and single radar coverage in others.…”
Section: Test Scenario Developmentmentioning
confidence: 99%
“…6 In ERAM Release 1 formal test, a linear predictor was used as the Test Predictor. Similar approaches to validate the issuance of an alert for non-conflict near LoS situations also make use of a linear predictor [7,8,10]. In ERAM formal and regression test, the velocity is computed using the central difference method from "ground truth" position points in the past up to the evaluation time.…”
Section: Test Predictor Operating On Truth Datamentioning
confidence: 99%
“…Such a definition avoids the need to define what constitutes a 'nuisance opportunity' or near encounter. This was presented as one of two False Alert rate definitions in references [7,8].…”
Section: Nuisance Ratementioning
confidence: 99%
“…5 [15]. This definition has been used in analyses of conflict probe [25] and was one of two metrics presented in [7,8]. An alternative approach to defining nuisance opportunities has been used at NASA Ames in research on TSAFE [26] whereby a near encounter is defined as a situation where the 1 minute dead-reckoning (based on track data but alternatively could use truth data when available) projects the aircraft to get within 6 nmi and 1200 ft, except if the aircraft are flying level and in conformance to their cleared and separated altitudes.…”
“…This approach relies on the use of a linear predictor operating on truth data to check the validity and timeliness of an alert. A similar approach is described in [7] and [8], using however smooth and interpolated track outputs instead of truth data.…”
Section: Introductionmentioning
confidence: 91%
“…For 3 The term "valid-late" has also been applied to such alerts [8] instance, ERAM had requirements to be able to perform surveillance processing over an area as large as 2000 nmi by 2000 nmi with a specified mix of short and long range radars providing multiple radar coverage in some areas and single radar coverage in others.…”
Section: Test Scenario Developmentmentioning
confidence: 99%
“…6 In ERAM Release 1 formal test, a linear predictor was used as the Test Predictor. Similar approaches to validate the issuance of an alert for non-conflict near LoS situations also make use of a linear predictor [7,8,10]. In ERAM formal and regression test, the velocity is computed using the central difference method from "ground truth" position points in the past up to the evaluation time.…”
Section: Test Predictor Operating On Truth Datamentioning
confidence: 99%
“…Such a definition avoids the need to define what constitutes a 'nuisance opportunity' or near encounter. This was presented as one of two False Alert rate definitions in references [7,8].…”
Section: Nuisance Ratementioning
confidence: 99%
“…5 [15]. This definition has been used in analyses of conflict probe [25] and was one of two metrics presented in [7,8]. An alternative approach to defining nuisance opportunities has been used at NASA Ames in research on TSAFE [26] whereby a near encounter is defined as a situation where the 1 minute dead-reckoning (based on track data but alternatively could use truth data when available) projects the aircraft to get within 6 nmi and 1200 ft, except if the aircraft are flying level and in conformance to their cleared and separated altitudes.…”
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