Location

SLU Location

To check the ANSS location or to compare the observed P-wave first motions to the moment tensor solution, P- and S-wave first arrival times were manually read together with the P-wave first motions. The subsequent output of the program elocate is given in the file elocate.txt. The first motion plot is shown below.

Location ANSS

The ANSS event ID is us6000b6wi and the event page is at https://earthquake.usgs.gov/earthquakes/eventpage/us6000b6wi/executive.

2020/07/30 15:04:11 36.250 -106.767 11.4 3.7 New Mexico

Focal Mechanism

 USGS/SLU Moment Tensor Solution
 ENS  2020/07/30 15:04:11:0  36.25 -106.77  11.4 3.7 New Mexico
 
 Stations used:
   AE.HANNA AE.W18A AE.X18A C0.LAMA C0.S22A C0.T25A IU.ANMO 
   N4.MSTX SC.121A SC.Y22A TX.PH02 TX.RTBA US.ISCO US.MVCO 
   US.SDCO US.WUAZ UU.HMU YX.UNM2 YX.UNM3 YX.UNM5 
 
 Filtering commands used:
   cut o DIST/3.3 -40 o DIST/3.3 +50
   rtr
   taper w 0.1
   hp c 0.03 n 3 
   lp c 0.06 n 3 
 
 Best Fitting Double Couple
  Mo = 3.51e+21 dyne-cm
  Mw = 3.63 
  Z  = 15 km
  Plane   Strike  Dip  Rake
   NP1      126    79   -134
   NP2       25    45   -15
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   3.51e+21     22     248
    N   0.00e+00     43     136
    P  -3.51e+21     39     357

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx    -1.67e+21
       Mxy     1.19e+21
       Mxz    -2.17e+21
       Myy     2.58e+21
       Myz    -1.01e+21
       Mzz    -9.08e+20
                                                     
                                                     
                                                     
                                                     
                     --------------                  
                 ---------------------#              
              -------------------------###           
             -------------   -----------###          
           --------------- P -----------#####        
          ###-------------   -----------######       
         #####---------------------------######      
        ########-------------------------#######     
        ##########-----------------------#######     
       #############--------------------#########    
       ###############------------------#########    
       ##################---------------#########    
       ####################------------##########    
        ###   ################--------##########     
        ### T ###################----###########     
         ##   #################################      
          #########################-----######       
           ######################------------        
             ##################------------          
              ###############-------------           
                 ########--------------              
                     --------------                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -9.08e+20  -2.17e+21   1.01e+21 
 -2.17e+21  -1.67e+21  -1.19e+21 
  1.01e+21  -1.19e+21   2.58e+21 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200730150411/index.html
        

Preferred Solution

The preferred solution from an analysis of the surface-wave spectral amplitude radiation pattern, waveform inversion or first motion observations is

      STK = 25
      DIP = 45
     RAKE = -15
       MW = 3.63
       HS = 15.0

The NDK file is 20200730150411.ndk The waveform inversion is preferred.

Moment Tensor Comparison

The following compares this source inversion to those provided by others. The purpose is to look for major differences and also to note slight differences that might be inherent to the processing procedure. For completeness the USGS/SLU solution is repeated from above.
SLU
USGSMWR
SLUFM
 USGS/SLU Moment Tensor Solution
 ENS  2020/07/30 15:04:11:0  36.25 -106.77  11.4 3.7 New Mexico
 
 Stations used:
   AE.HANNA AE.W18A AE.X18A C0.LAMA C0.S22A C0.T25A IU.ANMO 
   N4.MSTX SC.121A SC.Y22A TX.PH02 TX.RTBA US.ISCO US.MVCO 
   US.SDCO US.WUAZ UU.HMU YX.UNM2 YX.UNM3 YX.UNM5 
 
 Filtering commands used:
   cut o DIST/3.3 -40 o DIST/3.3 +50
   rtr
   taper w 0.1
   hp c 0.03 n 3 
   lp c 0.06 n 3 
 
 Best Fitting Double Couple
  Mo = 3.51e+21 dyne-cm
  Mw = 3.63 
  Z  = 15 km
  Plane   Strike  Dip  Rake
   NP1      126    79   -134
   NP2       25    45   -15
  Principal Axes:
   Axis    Value   Plunge  Azimuth
    T   3.51e+21     22     248
    N   0.00e+00     43     136
    P  -3.51e+21     39     357

 Moment Tensor: (dyne-cm)
    Component   Value
       Mxx    -1.67e+21
       Mxy     1.19e+21
       Mxz    -2.17e+21
       Myy     2.58e+21
       Myz    -1.01e+21
       Mzz    -9.08e+20
                                                     
                                                     
                                                     
                                                     
                     --------------                  
                 ---------------------#              
              -------------------------###           
             -------------   -----------###          
           --------------- P -----------#####        
          ###-------------   -----------######       
         #####---------------------------######      
        ########-------------------------#######     
        ##########-----------------------#######     
       #############--------------------#########    
       ###############------------------#########    
       ##################---------------#########    
       ####################------------##########    
        ###   ################--------##########     
        ### T ###################----###########     
         ##   #################################      
          #########################-----######       
           ######################------------        
             ##################------------          
              ###############-------------           
                 ########--------------              
                     --------------                  
                                                     
                                                     
                                                     
 Global CMT Convention Moment Tensor:
      R          T          P
 -9.08e+20  -2.17e+21   1.01e+21 
 -2.17e+21  -1.67e+21  -1.19e+21 
  1.01e+21  -1.19e+21   2.58e+21 


Details of the solution is found at

http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20200730150411/index.html
	
Regional Moment Tensor (Mwr)
Moment 4.852e+14 N-m
Magnitude 3.72 Mwr
Depth 14.0 km
Percent DC 85%
Half Duration -
Catalog US
Data Source US 1
Contributor US 1

Nodal Planes
Plane Strike Dip Rake
NP1 144° 53° -123°
NP2 11° 47° -54°

Principal Axes
Axis Value Plunge Azimuth
T 5.032e+14 N-m 3° 256°
N -0.383e+14 N-m 26° 165°
P -4.649e+14 N-m 64° 353°

        


First motions and takeoff angles from an elocate run.

Magnitudes

Given the availability of digital waveforms for determination of the moment tensor, this section documents the added processing leading to mLg, if appropriate to the region, and ML by application of the respective IASPEI formulae. As a research study, the linear distance term of the IASPEI formula for ML is adjusted to remove a linear distance trend in residuals to give a regionally defined ML. The defined ML uses horizontal component recordings, but the same procedure is applied to the vertical components since there may be some interest in vertical component ground motions. Residual plots versus distance may indicate interesting features of ground motion scaling in some distance ranges. A residual plot of the regionalized magnitude is given as a function of distance and azimuth, since data sets may transcend different wave propagation provinces.

ML Magnitude


Left: ML computed using the IASPEI formula for Horizontal components. Center: ML residuals computed using a modified IASPEI formula that accounts for path specific attenuation; the values used for the trimmed mean are indicated. The ML relation used for each figure is given at the bottom of each plot. Right: Residuals from new relation as a function of distance and azimuth.


Left: ML computed using the IASPEI formula for Vertical components (research). Center: ML residuals computed using a modified IASPEI formula that accounts for path specific attenuation; the values used for the trimmed mean are indicated. The ML relation used for each figure is given at the bottom of each plot. Right: Residuals from new relation as a function of distance and azimuth.

Context

The left panel of the next figure presents the focal mechanism for this earthquake (red) in the context of other nearby events (blue) in the SLU Moment Tensor Catalog. The right panel shows the inferred direction of maximum compressive stress and the type of faulting (green is strike-slip, red is normal, blue is thrust; oblique is shown by a combination of colors). Thus context plot is useful for assessing the appropriateness of the moment tensor of this event.

Waveform Inversion using wvfgrd96

The focal mechanism was determined using broadband seismic waveforms. The location of the event (star) and the stations used for (red) the waveform inversion are shown in the next figure.
Location of broadband stations used for waveform inversion

The program wvfgrd96 was used with good traces observed at short distance to determine the focal mechanism, depth and seismic moment. This technique requires a high quality signal and well determined velocity model for the Green's functions. To the extent that these are the quality data, this type of mechanism should be preferred over the radiation pattern technique which requires the separate step of defining the pressure and tension quadrants and the correct strike.

The observed and predicted traces are filtered using the following gsac commands:

cut o DIST/3.3 -40 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.06 n 3 
The results of this grid search are as follow:

           DEPTH  STK   DIP  RAKE   MW    FIT
WVFGRD96    1.0   110    45   -85   3.35 0.3859
WVFGRD96    2.0   105    45   -85   3.43 0.4294
WVFGRD96    3.0    25    70    -5   3.42 0.4047
WVFGRD96    4.0   305    75   -60   3.52 0.4086
WVFGRD96    5.0   310    80   -60   3.52 0.4375
WVFGRD96    6.0   310    80   -55   3.51 0.4619
WVFGRD96    7.0   315    85   -50   3.51 0.4796
WVFGRD96    8.0    25    35   -20   3.58 0.5067
WVFGRD96    9.0    25    40   -20   3.59 0.5331
WVFGRD96   10.0    25    40   -25   3.60 0.5558
WVFGRD96   11.0    25    40   -25   3.60 0.5722
WVFGRD96   12.0    25    45   -25   3.62 0.5848
WVFGRD96   13.0    25    45   -20   3.62 0.5932
WVFGRD96   14.0    25    45   -20   3.62 0.5966
WVFGRD96   15.0    25    45   -15   3.63 0.5966
WVFGRD96   16.0    25    45   -15   3.63 0.5943
WVFGRD96   17.0    40    45    20   3.64 0.5911
WVFGRD96   18.0    40    50    20   3.65 0.5881
WVFGRD96   19.0    40    50    20   3.66 0.5835
WVFGRD96   20.0    40    50    20   3.66 0.5775
WVFGRD96   21.0    40    50    20   3.67 0.5687
WVFGRD96   22.0    40    50    20   3.68 0.5599
WVFGRD96   23.0    40    50    20   3.68 0.5505
WVFGRD96   24.0    45    50    25   3.69 0.5406
WVFGRD96   25.0    45    50    25   3.69 0.5302
WVFGRD96   26.0    45    50    25   3.70 0.5194
WVFGRD96   27.0    45    50    25   3.71 0.5082
WVFGRD96   28.0    45    50    25   3.71 0.4965
WVFGRD96   29.0    50    45    25   3.71 0.4845

The best solution is

WVFGRD96   15.0    25    45   -15   3.63 0.5966

The mechanism corresponding to the best fit is
Figure 1. Waveform inversion focal mechanism

The best fit as a function of depth is given in the following figure:

Figure 2. Depth sensitivity for waveform mechanism

The comparison of the observed and predicted waveforms is given in the next figure. The red traces are the observed and the blue are the predicted. Each observed-predicted component is plotted to the same scale and peak amplitudes are indicated by the numbers to the left of each trace. A pair of numbers is given in black at the right of each predicted traces. The upper number it the time shift required for maximum correlation between the observed and predicted traces. This time shift is required because the synthetics are not computed at exactly the same distance as the observed, the velocity model used in the predictions may not be perfect and the epicentral parameters may be be off. A positive time shift indicates that the prediction is too fast and should be delayed to match the observed trace (shift to the right in this figure). A negative value indicates that the prediction is too slow. The lower number gives the percentage of variance reduction to characterize the individual goodness of fit (100% indicates a perfect fit).

The bandpass filter used in the processing and for the display was

cut o DIST/3.3 -40 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.06 n 3 
Figure 3. Waveform comparison for selected depth. Red: observed; Blue - predicted. The time shift with respect to the model prediction is indicated. The percent of fit is also indicated. The time scale is relative to the first trace sample.

Focal mechanism sensitivity at the preferred depth. The red color indicates a very good fit to the waveforms. Each solution is plotted as a vector at a given value of strike and dip with the angle of the vector representing the rake angle, measured, with respect to the upward vertical (N) in the figure.

A check on the assumed source location is possible by looking at the time shifts between the observed and predicted traces. The time shifts for waveform matching arise for several reasons:

Assuming only a mislocation, the time shifts are fit to a functional form:

 Time_shift = A + B cos Azimuth + C Sin Azimuth

The time shifts for this inversion lead to the next figure:

The derived shift in origin time and epicentral coordinates are given at the bottom of the figure.

Velocity Model

The WUS.model used for the waveform synthetic seismograms and for the surface wave eigenfunctions and dispersion is as follows (The format is in the model96 format of Computer Programs in Seismology).

MODEL.01
Model after     8 iterations
ISOTROPIC
KGS
FLAT EARTH
1-D
CONSTANT VELOCITY
LINE08
LINE09
LINE10
LINE11
      H(KM)   VP(KM/S)   VS(KM/S) RHO(GM/CC)         QP         QS       ETAP       ETAS      FREFP      FREFS
     1.9000     3.4065     2.0089     2.2150  0.302E-02  0.679E-02   0.00       0.00       1.00       1.00    
     6.1000     5.5445     3.2953     2.6089  0.349E-02  0.784E-02   0.00       0.00       1.00       1.00    
    13.0000     6.2708     3.7396     2.7812  0.212E-02  0.476E-02   0.00       0.00       1.00       1.00    
    19.0000     6.4075     3.7680     2.8223  0.111E-02  0.249E-02   0.00       0.00       1.00       1.00    
     0.0000     7.9000     4.6200     3.2760  0.164E-10  0.370E-10   0.00       0.00       1.00       1.00    
Last Changed Thu Apr 25 07:59:10 PM CDT 2024