Location

Location ANSS

The ANSS event ID is ci37299263 and the event page is at https://earthquake.usgs.gov/earthquakes/eventpage/ci37299263/executive.

2016/01/24 15:32:16 34.697 -116.239 2.6 4.11 California

Focal Mechanism

USGS/SLU Moment Tensor Solution ENS 2016/01/24 15:32:16:0 34.70 -116.24 2.6 4.1 California Stations used: AE.W13A AZ.FRD AZ.PFO AZ.RRSP AZ.SMER AZ.SND CI.ADO CI.BAR CI.BBR CI.BC3 CI.BEL CI.BFS CI.CCC CI.CGO CI.CHF CI.CWC CI.DAN CI.DEC CI.DGR CI.DJJ CI.EDW2 CI.FOX2 CI.FUR CI.GLA CI.GMR CI.GRA CI.GSC CI.HEC CI.ISA CI.LMR2 CI.LPC CI.MOP CI.MPM CI.MTP CI.MUR CI.MWC CI.NEE2 CI.OSI CI.PASC CI.PMD CI.RRX CI.RVR CI.SHO CI.SLA CI.SPG2 CI.TIN CI.TUQ CI.USC CI.VCS CI.VTV CI.WCS2 NN.LCH NN.SHP NN.V12A PY.BPH01 PY.BPH10 YN.GVAR1 YN.JF00 YN.RHIL YN.TR01 Filtering commands used: cut o DIST/3.3 -20 o DIST/3.3 +50 rtr taper w 0.1 hp c 0.03 n 3 lp c 0.07 n 3 Best Fitting Double Couple Mo = 1.10e+22 dyne-cm Mw = 3.96 Z = 11 km Plane Strike Dip Rake NP1 151 72 154 NP2 250 65 20 Principal Axes: Axis Value Plunge Azimuth T 1.10e+22 31 109 N 0.00e+00 58 299 P -1.10e+22 5 202 Moment Tensor: (dyne-cm) Component Value Mxx -8.54e+21 Mxy -6.23e+21 Mxz -7.76e+20 Myy 5.67e+21 Myz 4.92e+21 Mzz 2.87e+21 -------------- #--------------------- ####------------------------ #####------------------------- #######--------------------------- #########--------------------------- ##########-----------------#######---- ############-------##################### #############--######################### ############---########################### #########------########################### #######---------########################## #####------------################ ###### ##---------------############### T ##### #------------------############# ##### -------------------################### -------------------################# --------------------############## -------------------########### ----- ------------######## -- P ---------------## ------------- Global CMT Convention Moment Tensor: R T P 2.87e+21 -7.76e+20 -4.92e+21 -7.76e+20 -8.54e+21 6.23e+21 -4.92e+21 6.23e+21 5.67e+21 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20160124153216/index.html

Preferred Solution

      STK = 250
      DIP = 65
     RAKE = 20
       MW = 3.96
       HS = 11.0

The NDK file is 20160124153216.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

SCAL

USGS/SLU Moment Tensor Solution ENS 2016/01/24 15:32:16:0 34.70 -116.24 2.6 4.1 California Stations used: AE.W13A AZ.FRD AZ.PFO AZ.RRSP AZ.SMER AZ.SND CI.ADO CI.BAR CI.BBR CI.BC3 CI.BEL CI.BFS CI.CCC CI.CGO CI.CHF CI.CWC CI.DAN CI.DEC CI.DGR CI.DJJ CI.EDW2 CI.FOX2 CI.FUR CI.GLA CI.GMR CI.GRA CI.GSC CI.HEC CI.ISA CI.LMR2 CI.LPC CI.MOP CI.MPM CI.MTP CI.MUR CI.MWC CI.NEE2 CI.OSI CI.PASC CI.PMD CI.RRX CI.RVR CI.SHO CI.SLA CI.SPG2 CI.TIN CI.TUQ CI.USC CI.VCS CI.VTV CI.WCS2 NN.LCH NN.SHP NN.V12A PY.BPH01 PY.BPH10 YN.GVAR1 YN.JF00 YN.RHIL YN.TR01 Filtering commands used: cut o DIST/3.3 -20 o DIST/3.3 +50 rtr taper w 0.1 hp c 0.03 n 3 lp c 0.07 n 3 Best Fitting Double Couple Mo = 1.10e+22 dyne-cm Mw = 3.96 Z = 11 km Plane Strike Dip Rake NP1 151 72 154 NP2 250 65 20 Principal Axes: Axis Value Plunge Azimuth T 1.10e+22 31 109 N 0.00e+00 58 299 P -1.10e+22 5 202 Moment Tensor: (dyne-cm) Component Value Mxx -8.54e+21 Mxy -6.23e+21 Mxz -7.76e+20 Myy 5.67e+21 Myz 4.92e+21 Mzz 2.87e+21 -------------- #--------------------- ####------------------------ #####------------------------- #######--------------------------- #########--------------------------- ##########-----------------#######---- ############-------##################### #############--######################### ############---########################### #########------########################### #######---------########################## #####------------################ ###### ##---------------############### T ##### #------------------############# ##### -------------------################### -------------------################# --------------------############## -------------------########### ----- ------------######## -- P ---------------## ------------- Global CMT Convention Moment Tensor: R T P 2.87e+21 -7.76e+20 -4.92e+21 -7.76e+20 -8.54e+21 6.23e+21 -4.92e+21 6.23e+21 5.67e+21 Details of the solution is found at http://www.eas.slu.edu/eqc/eqc_mt/MECH.NA/20160124153216/index.html

Scientific - Focal Mechanism Data Source CI1 Catalog CI (ci37299263) Data Source CI1 Contributor CI1 Nodal Planes Plane Strike Dip Rake NP1 305 66 103 NP2 94 27 62 TMTS Moment 1.790e+15 N-m Magnitude 4.10 Depth 5.0 km Percent DC 93% Half Duration – Catalog CI (ci37299263) Data Source CI1 Contributor CI1 Nodal Planes Plane Strike Dip Rake NP1 191 50 -104 NP2 32 42 -74 Principal Axes Axis Value Plunge Azimuth T 1.757 4 291 N 0.064 10 200 P -1.822 79 43

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 M_L by application of the respective IASPEI formulae. As a research study, the linear distance term of the IASPEI formula for M_L is adjusted to remove a linear distance trend in residuals to give a regionally defined M_L. The defined M_L 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

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 -20 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.07 n 3 

           DEPTH  STK   DIP  RAKE   MW    FIT
WVFGRD96    1.0    55    60   -40   3.63 0.3463
WVFGRD96    2.0    50    50   -45   3.78 0.4630
WVFGRD96    3.0    40    45   -60   3.87 0.5241
WVFGRD96    4.0    40    45   -60   3.90 0.5568
WVFGRD96    5.0    40    45   -60   3.92 0.5676
WVFGRD96    6.0    55    55   -35   3.88 0.5630
WVFGRD96    7.0    65    70   -15   3.87 0.5648
WVFGRD96    8.0    55    55   -35   3.94 0.5796
WVFGRD96    9.0   250    65    20   3.93 0.5781
WVFGRD96   10.0   250    65    20   3.94 0.5834
WVFGRD96   11.0   250    65    20   3.96 0.5844
WVFGRD96   12.0   250    65    20   3.97 0.5822
WVFGRD96   13.0   250    70    20   3.98 0.5781
WVFGRD96   14.0   250    70    20   3.99 0.5717
WVFGRD96   15.0   250    70    20   4.00 0.5645
WVFGRD96   16.0   250    70    20   4.01 0.5558
WVFGRD96   17.0   250    70    20   4.02 0.5466
WVFGRD96   18.0   250    70    20   4.03 0.5364
WVFGRD96   19.0   250    70    20   4.03 0.5258
WVFGRD96   20.0   250    70    20   4.04 0.5150
WVFGRD96   21.0   250    70    20   4.05 0.5039
WVFGRD96   22.0   250    70    20   4.06 0.4927
WVFGRD96   23.0   250    70    20   4.06 0.4813
WVFGRD96   24.0   250    70    20   4.07 0.4704
WVFGRD96   25.0   250    70    20   4.08 0.4593
WVFGRD96   26.0   250    70    20   4.08 0.4482
WVFGRD96   27.0   250    70    20   4.09 0.4374
WVFGRD96   28.0   250    70    20   4.09 0.4264
WVFGRD96   29.0   250    70    20   4.10 0.4162

The best solution is

WVFGRD96   11.0   250    65    20   3.96 0.5844

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 -20 o DIST/3.3 +50
rtr
taper w 0.1
hp c 0.03 n 3 
lp c 0.07 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:

• The origin time and epicentral distance are incorrect
• The velocity model used for the inversion is incorrect
• The velocity model used to define the P-arrival time is not the same as the velocity model used for the waveform inversion (assuming that the initial trace alignment is based on the P arrival time)

 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