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Wavelet Analysis of Cockpit Voice Recorder Data.

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Presentation on theme: "Wavelet Analysis of Cockpit Voice Recorder Data."— Presentation transcript:

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7 Wavelet Analysis of Cockpit Voice Recorder Data

8 Project Responsibilities Team Leader Digitize CVR Data, Develop Test Signals

9 Project Responsibilities Code Developer Develop Wavelet source code

10 Project Responsibilities Research Research Wavelet Theory

11 Overview Project Background CVR Basics & Recording Theory Wavelet Parameters Silent Track Analysis

12 Project Background 1991 Beech 1900C Twin Turboprop Accident

13 Accident Location Project Background

14 Right engine mount failed Engine separated and struck empennage Aircraft broke apart in flight Recovered CVR with last 30 min of audio Project Background

15 Engine Mount Location

16 Accident Animation

17 Project Goals Digitize CVR recording Isolate tube failure location Develop Wavelet analysis program Perform Wavelet Analysis on CVR data

18 Digitize CVR Data

19 2146:29 INT-2 ah once your established inbound right you're good to what? 2146:34 INT-1 oh #. 2146:34 CAM ((sound of altitude alert chime)) 2146:35 INT-2 stop one thing at a time. you're in a bad situation so correct one thing first. CVR Transcript and Tape Catastrophic Event

20 Goldwave Analysis Goldwave is a digital audio editing program.

21 Goldwave Analysis Windowed Fourier Transform

22 Goldwave Analysis Windowed Fourier Results These frequencies match those found by past research.

23 Goldwave Analysis Final portion of CVR recording

24 Integral Transformation Theory What is it? Transforms a function from one space to another depending on the transfer function.

25 The Fourier Transform Signal processing tool that takes a signal and tells us what frequencies are within that signal.

26 The Wavelet Transform Determines the frequency spectrum as a function of time.

27 Morlet Wavelet Equations Morlet Wavelet Scaling/Translation Function Wavelet Transform

28 Triboelectric Effect Frictional motion creates static electricity Aircraft wires vibrate during flight Vibrations generate static electricity CVR records static electricity

29 Develop Wavelet Computer Code Obtained existing Wavelet code from C. Torrence and G. Compo Created interface allowing use of Wavelet code Experimented with effect of input parameters

30 Important Input Parameters Wo – Effects Wavelet width dj – Effects scale width mother – Type of Wavelet Transform Parameters : Scale Parameters: J1 – # of Scales So – Base Scale

31 An Example

32 Fourier Analysis

33 Wavelet Analysis of Test Signal Morlet Wavelet Wo = 6 dj =.25 Wo = 24 dj =.25 Wo = 24 dj =.025

34 DOG Wavelet Wavelet Analysis of Test Signal m = 2 dj =.025

35 Wavelet Display Test Wo = 6 dj =.125 Morlet Wavelet

36 Scale Parameter Equations Minimum Scale Size Maximum Wavenumber Beat Phenomenon Edge Effects and Tone Width Wavelet Code Improvements

37 Scale Parameter Equations Base Scale Size Number of Scales

38 Minimum Scale Size

39 Maximum Wavenumber 5 Hz Test Tone

40 Beat Phenomenon 50 Hz & 52 Hz Tones

41 Wavelet Analysis 4p Propeller Mode

42 Wavelet Analysis Right Engine Turbine

43 Future Work Continue verifying code consistency Obtain controlled triboelectric test data Investigate other crash explanations

44 Acknowledgements Dr. Ronald Stearman Pete Moss – UT School of Music Chris Garland Javier Fuentealba Marcus Kruger

45 Questions


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