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A Trajectory Algorithm to Support En Route and Terminal Area Self-Spacing Concepts: Fifth RevisionThis document describes an algorithm for the generation of a four dimensional trajectory. Input data for this algorithm are similar to an augmented Standard Terminal Arrival (STAR) with the augmentation in the form of altitude or speed crossing restrictions at waypoints on the route. The algorithm calculates the altitude, speed, along path distance, and along path time for each of these waypoints. Wind data at each of these waypoints are also used for the calculation of ground speed and turn radius. This revision of the algorithm now accommodates linear decelerations between two speed-constrained waypoints. While this modification may appear trivial, the calculation of the deceleration rate cannot be accomplished using a closed-form solution. An iterative solution was developed that allowed for the variability of path distance due to speed influence on turn radii, Mach-CAS transition altitude, and the impact of wind on ground speed in calculating an accurate deceleration value.
Document ID
20230013358
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Terence S. Abbott
(Distinguished Research Associates Hampton, Virginia, United States)
Date Acquired
September 13, 2023
Publication Date
October 1, 2023
Subject Category
Computer Programming and Software
Air Transportation and Safety
Mathematical and Computer Sciences (General)
Report/Patent Number
NASA/CR–2018-219828
NASA/CR-2014-218288
NASA/CR-2010-216204
NASA/CR-2007-214899
Funding Number(s)
WBS: 395872.04.40.07.04
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Aircraft Operations
Approach Spacing
Aircraft Systems
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