Accuracy Assessment of Regime Recognition Algorithms Using Confusion Matrix

SM_2015_CBM-1407

2/9/2015

Authors
Abstract
Content

An accurate characterization of the operational flight regime is a key characteristic of the CBM system. In order to establish regime recognition algorithms as the basis for retirement time of aircraft components, algorithms should be validated through a rigorous verification and validation process using dedicated flight test data with sufficient flight conditions and time. For military aircraft, ADS-79D Appendix B provides detailed guidance for validation of regime recognition algorithms, including their accuracy requirements: "… such as 97% or greater recognition of the actual flight regimes,…", and "… any unrecognized regimes would introduce less than 0.5% under-prediction of fatigue damage fraction based on the design usage spectrum." It has been shown very challenging to meet this 97% accuracy requirement due to limitations with the current regime recognition algorithms. One of the major issues encountered is that multiple regimes are identified by the code for a supposedly single regime time. It is seem intuitive that more than one single regime are recognized during the changing flight conditions particularly for transient maneuvers, when a time sliced regime recognition logic is implemented even with the help of more advanced logic added. As a way to alleviate the stringent measure of "black and white" criteria, the confusion matrix is studied with correlation factors using regime load pattern recognitions to establish a method for better assessment of regime recognition accuracy, and eventually, better assessment of fatigue damage fraction. The study compares the improved regime recognition accuracy using extensive flight survey data.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_2015_CBM-1407
Citation
Hong, C., "Accuracy Assessment of Regime Recognition Algorithms Using Confusion Matrix," Airworthiness, CBM and HUMS - Huntsville, Alabama 2015, Huntsville, Alabama, February 9, 2015, https://doi.org/10.4050/SM_2015_CBM-1407.
Additional Details
Publisher
Published
2/9/2015
Product Code
SM_2015_CBM-1407
Content Type
Technical Paper
Language
English