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原文传递 Evaluation of a Flight Deck Interval Management Algorithm Including Delayed Target Trajectories

题名：	Evaluation of a Flight Deck Interval Management Algorithm Including Delayed Target Trajectories
作者：	Swieringa, K. A.; Underwood, M. C.; Barmore, B.; Leonard, R. D.
关键词：	Air traffic control##Flight management systems##Airspace##Algorithms##Aircraft approach spacing##Delay##Trajectories##Technology assessment##Point to point communication##Arrivals##Experiment design##Wind direction##Velocity distribution##Position errors##Software development tools##Speed control##Computerized simulation##Wind velocity##Standard deviation##Nasa programs##Research and development##Systems integration##Dynamic models##Landing simulation##Aircraft models##
摘要：	NASA's first Air Traffic Management (ATM) Technology Demonstration (ATD-1) was created to facilitate the transition of mature air traffic management technologies from the laboratory to operational use. The technologies selected for demonstration are the Traffic Management Advisor with Terminal Metering (TMA-TM), which provides precise timebased scheduling in the terminal airspace; Controller Managed Spacing (CMS), which provides controllers with decision support tools enabling precise schedule conformance; and Interval Management (IM), which consists of flight deck automation that enables aircraft to achieve or maintain precise in-trail spacing. During high demand operations, TMA-TM may produce a schedule and corresponding aircraft trajectories that include delay to ensure that a particular aircraft will be properly spaced from other aircraft at each schedule waypoint. These delayed trajectories are not communicated to the automation onboard the aircraft, forcing the IM aircraft to use the published speeds to estimate the target aircraft's estimated time of arrival. As a result, the aircraft performing IM operations may follow an aircraft whose TMA-TM generated trajectories have substantial speed deviations from the speeds expected by the spacing algorithm. Previous spacing algorithms were not designed to handle this magnitude of uncertainty. A simulation was conducted to examine a modified spacing algorithm with the ability to follow aircraft flying delayed trajectories. The simulation investigated the use of the new spacing algorithm with various delayed speed profiles and wind conditions, as well as several other variables designed to simulate real-life variability. The results and conclusions of this study indicate that the new spacing algorithm generally exhibits good performance; however, some types of target aircraft speed profiles can cause the spacing algorithm to command less than optimal speed control behavior.
总页数：	11
报告类型：	科技报告