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Wake Vortex Inverse Model User's GuideNorthWest Research Associates (NWRA) has developed an inverse model for inverting landing aircraft vortex data. The data used for the inversion are the time evolution of the lateral transport position and vertical position of both the port and starboard vortices. The inverse model performs iterative forward model runs using various estimates of vortex parameters, vertical crosswind profiles, and vortex circulation as a function of wake age. Forward model predictions of lateral transport and altitude are then compared with the observed data. Differences between the data and model predictions guide the choice of vortex parameter values, crosswind profile and circulation evolution in the next iteration. Iterations are performed until a user-defined criterion is satisfied. Currently, the inverse model is set to stop when the improvement in the rms deviation between the data and model predictions is less than 1 percent for two consecutive iterations. The forward model used in this inverse model is a modified version of the Shear-APA model. A detailed description of this forward model, the inverse model, and its validation are presented in a different report (Lai, Mellman, Robins, and Delisi, 2007). This document is a User's Guide for the Wake Vortex Inverse Model. Section 2 presents an overview of the inverse model program. Execution of the inverse model is described in Section 3. When executing the inverse model, a user is requested to provide the name of an input file which contains the inverse model parameters, the various datasets, and directories needed for the inversion. A detailed description of the list of parameters in the inversion input file is presented in Section 4. A user has an option to save the inversion results of each lidar track in a mat-file (a condensed data file in Matlab format). These saved mat-files can be used for post-inversion analysis. A description of the contents of the saved files is given in Section 5. An example of an inversion input file, with preferred parameters values, is given in Appendix A. An example of the plot generated at a normal completion of the inversion is shown in Appendix B.
Document ID
20100003352
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Lai, David
(Northwest Research Associates, Inc. Redmond, WA, United States)
Delisi, Donald
(Northwest Research Associates, Inc. Redmond, WA, United States)
Date Acquired
August 25, 2013
Publication Date
October 2, 2008
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
LF99-9840
NWRA-SEA-08-R351R1
Report Number: LF99-9840
Report Number: NWRA-SEA-08-R351R1
Funding Number(s)
CONTRACT_GRANT: TO6-6000-NWRA
OTHER: Subtask 3.3.2
CONTRACT_GRANT: NNL06AC78T
WBS: WBS 411931.02.61.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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