tsaregular
Regular signal of a time-synchronous averaged signal
Syntax
Description
computes the regular signal Y
= tsaregular(X
,fs
,rpm
,orderList
)Y
of the time-synchronous averaged (TSA)
signal vector X
using sampling rate fs
, the
rotational speed rpm
, and the orders to be retained
orderList
. Y
is computed by retaining the
primary frequency, the components in orderList
, and their respective
harmonics from X
. You can use Y
to further
extract condition indicators of rotating machinery for predictive maintenance. For
example, extracting the FM0 indicator from Y
is useful in identifying major changes such as gear tooth breakage or heavy wear in a gear
box.
___ = tsaregular(___,
allows you to specify additional parameters using one or more name-value pair arguments.
You can use this syntax with any of the previous input and output arguments.Name,Value
)
tsaregular(___)
with no output arguments plots the
time-domain and frequency-domain plots of the raw and regular TSA signals.
Examples
Input Arguments
Output Arguments
Algorithms
Regular Signal
The regular signal is computed from the TSA signal by retaining the following from the signal spectrum:
Shaft frequency and its harmonics
Gear meshing frequencies and their harmonics
Optionally, the sidebands specified in '
NumSidebands
' at the gear meshing frequencies and their harmonics
tsaregular
uses a bandwidth equal to the shaft speed times the value of
'NumSidebands
', around the frequencies of interest, to compute
Y
from the TSA signal. The regular signal is related to the residual
signal through the equation . If the first-order sidebands are retained in the regular signal, then, .
Amplitude Spectrum
The amplitude spectrum of the regular signal is computed as follows,
Here, Y
is the regular signal.
References
[1] McFadden, P.D. "Examination of a Technique for the Early Detection of Failure in Gears by Signal Processing of the Time Domain Average of the Meshing Vibration." Aero Propulsion Technical Memorandum 434. Melbourne, Australia: Aeronautical Research Laboratories, Apr. 1986.
[2] Večeř, P., Marcel Kreidl, and R. Šmíd. "Condition Indicators for Gearbox Monitoring Systems." Acta Polytechnica 45.6 (2005), pages 35-43.
[3] Zakrajsek, J. J., Townsend, D. P., and Decker, H. J. "An Analysis of Gear Fault Detection Methods as Applied to Pitting Fatigue Failure Data." Technical Memorandum 105950. NASA, Apr. 1993.
[4] Zakrajsek, James J. "An investigation of gear mesh failure prediction techniques." National Aeronautics and Space Administration Cleveland OH Lewis Research Center, 1989. No. NASA-E-5049.
Extended Capabilities
Version History
Introduced in R2018b