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Performance Evaluation of Evasion Maneuvers for Parallel Approach Collision AvoidanceCurrent plans for independent instrument approaches to closely spaced parallel runways call for an automated pilot alerting system to ensure separation of aircraft in the case of a "blunder," or unexpected deviation from the a normal approach path. Resolution advisories by this system would require the pilot of an endangered aircraft to perform a trained evasion maneuver. The potential performance of two evasion maneuvers, referred to as the "turn-climb" and "climb-only," was estimated using an experimental NASA alerting logic (AILS) and a computer simulation of relative trajectory scenarios between two aircraft. One aircraft was equipped with the NASA alerting system, and maneuvered accordingly. Observation of the rates of different types of alerting failure allowed judgement of evasion maneuver performance. System Operating Characteristic (SOC) curves were used to assess the benefit of alerting with each maneuver.
Document ID
20000085966
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Winder, Lee F.
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Kuchar, James K.
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Waller, Marvin
Date Acquired
September 7, 2013
Publication Date
August 1, 2000
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.26:210099
NASA/CR-2000-210099
Report Number: NAS 1.26:210099
Report Number: NASA/CR-2000-210099
Funding Number(s)
CONTRACT_GRANT: NAG1-1974
PROJECT: RTOP 576-02-11-17
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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