october 2003 1 the woomera infrasound and seismic experiment david brown 1 ; clive collins 1 ; brian...
TRANSCRIPT
October 2003
1
The Woomera Infrasound and
Seismic Experiment
David Brown1; Clive Collins1; Brian Kennett2
1. Geoscience Australia2. Australian National University
Geological Survey of CanadaAustralian Dept. of Defence
October 2003
2
Introduction
The Woomera Experimento An international explosives trial held at Woomera, South Australia, in September, October 2002
o Conducted for defence research by:• UK Ministry of Defence• Australian Department of Defence
o Purpose:o ammunition stewardship program
o Participation by:• Canada• Netherlands• Norway• USA• Singapore
o Two explosions:• 27000 kg ammunition• 5000 kg ammunition
o Portable network of sensors was deployed:• 2 three-sensor infrasound arrays• 18 seismometers
IS07
October 2003
3
Woomera
Broken Hill
Introduction
167m
315m
1165m
900 m
Flinders Ranges
October 2003
4
Explosion Date (UT) Time (UT) Charge Size(kg)
Latitude(deg)
Longitude(deg)
1 20/09/2002 00:38:02.79 ± 0.06 27,050 -31.0108 136.7756
2 07/10/2002 01:08:04.39 ± 0.03 5,000 -31.0134 136.7857
Source Information
The Source
October 2003
The Source
Earthen walls 3 sidesConcrete roof
Explosives ContainerInstruments, tamping
October 2003
The Source
Some statistics
for a block of rubble
T = 33.57 sec = 508 m
V = 165.2 m/sH = 1380.5 m= 84.7 deg
27000 kg shot
Shock waveShock wave
October 2003
7
The Source
Norwegian house Australian house
October 2003
8
Station Distance(km)
Backazimuth(deg)
Sensor
IS07 1257 167.7 8 x MB2000
BH 467 283.0 3 x MB2000
OOD 476 161.1 3 x MB2000
Infrasound Receiver Information
StationDistance
(km)Backazimuth
(deg) Sensor
W660W 0.7 99.1 L4C HSA3
W660S 0.7 355.1 L4C HSA3
W04K 4.0 289.4 Guralp CMGT240
W08K 8.1 292.0 Guralp CMGT240
W12K 12.5 298.4 Guralp CMGT240
W16K 16.3 309.6 Guralp CMGT240
24KM 24.1 346.9 Guralp CMGT240
W32K 32.1 348.7 Guralp CMGT240
W48K 48.5 333.0 Guralp CMGT240
W64K 64.6 330.2 Guralp CMGT240
W72K 72.4 331.3 Guralp CMGT240
W84K 84.4 331.9 Guralp CMGT240
W100K 100.5 330.4 Guralp CMGT240
W125K 124.9 330.1 Guralp CMGT240
W150K 151.7 333.0 Guralp CMGT240
W175K 175.2 331.8 Guralp CMGT240
W200K 196.8 329.8 Guralp CMGT240
W250K 251.5 319.5 Guralp CMGT240
Seismic Receiver Information
Receiver Information
October 2003
Spectrogram: 20,000 lb Chemical Explosion @ 250 km 180 deg. backazimuth
• Broad-band signal• signal duration: 0.6 min• dominant period 1.6 sec• drop-off frequency:
– 6db down: > 2.0 Hz– 12 db down > 2.0 Hz
• Fstat– @ max SNR: 4.3– @Max Power: 21.5
• Frequency:– @max SNR 2.0 Hz– @max Power 0.47 Hz
• Need to design a 3-sensor array with maximum capability around 0.5 Hz. ie, average intersensor spacing of around 330 m.
Receiver Information
October 2003
10
Receiver Information
Broken Hill Station Finite-frequency array response
October 2003
11
Broken Hill Station
Receiver Information
October 2003
12
Receiver Information
Oodnadatta StationFinite-frequency array response
October 2003
13
Oodnadatta Station
Receiver Information
October 2003
14
Receiver Information
IS07 StationFinite-frequency array response
October 2003
15
Receiver Information
October 2003
16
The Signals
Broken Hill Station 27000 kg
October 2003
17
line Horizontal
velocity
m/s
H 340
A 310
B 300
C 290
D 280
E 270
F 260
G 250
The Signals
Broken Hill Station 27000 kg
0.8 – 3.2 Hz
October 2003
18
342 m/s289 deg
354 m/s290 deg
348 m/s290 deg
454 m/s256 deg 477 m/s
257 deg490 m/s241 deg
The Signals
Broken Hill Station 27000 kg
October 2003
19
line Horizontal
velocity
m/s
A 320
B 310
C 300
The Signals
IS07 27000 kg 352 m/s167 deg
October 2003
20
The Signals
Oodnadatta Station 27000 kg
line Horizontal
velocity
m/s
A 340
B 330
C 320
0.8 – 3.2 Hz
October 2003
21
The Signals
Broken Hill Station 5000 kg
line Horizontal
velocity
m/s
A 350
B 340
C 330
0.4 – 1.6 Hz
October 2003
22
GA Infrasonic Processing for CTBT monitoring
Infrasonic Processing at Geoscience Australiao Will process 5 IMS stations: IS03, IS04, IS05, IS06, IS07o Will observe the following processing philosophy
Single station processing: Seeking significant signals on individual stations
INFERAutomatic detector
detection
Interactive Analysisscanning
DISCINSimple discrimination criteria
arrival
Interactive Analysisreview
arrival
Automatic internal alert notification
rawdata
DISCEXHigh-level discrimination procedures
Manual external alert notification
duration > 2 minutesFstat > 10.0SNR > 1.5
Knowledge of local sources
SH investigation
Radionuclide investigation
Source Characterization study
57 days38185 detects 98 arrivals
1 arrival
October 2003
Signal parameter estimation at sparse arrays• Global minimisation of the misfit between theoretical and stacked beam powers• theoretical side-lobe pattern will be imprinted on the stacked beam power
ωω
ω
ωdeS
j
i j∫ ∑Δ⋅
=2
1
2
),(sr
sp
p
i
piip BSM
/181
1
)(),(81
1)( ⎟⎟
⎠
⎞⎜⎜⎝
⎛−= ∑
=sspp
ωωω
ω
ωdexB
j
ij
j∫ ∑⋅
=2
1
2
)(ˆ)(pr
p
Define broad-band theoretical array response to be
Define broad-band stacked beam-power to be
Define the misfit function using an norm as pL
Use the Sambridge Neighbourhood Algorithm to converge to the region of best fit.
GA Infrasonic Processing for CTBT monitoring
October 2003
Array response• Beam power as a function of slowness for I07AU array • Zero slowness • finite frequency signal centred at 0.875 Hz• 9 x 9 = 81 beams were used• maximum beam power centred on zero slowness
3
3
-3
-3
Sx (s/km)
Sy(s/km)
Signal Reception and Detection: Sparse Arrays
GA Infrasonic Processing for CTBT monitoring
October 2003
0 720 1440 2160 2880 3600
Time (sec)
Synthetic implant, azimuth, 128 deg. 3
-3
-3
3
Sx (s/km)
Sy
N
S
EWArray response• Beam power as a function of slowness for I07AU array with implanted signal• 9 x 9 = 81 beams were used• 0.875 Hz• maximum beam power centred on slowness corresponding to the implant azimuth (128 deg)
Slowness plane
Signal Reception and Detection: Sparse Arrays
GA Infrasonic Processing for CTBT monitoring
October 2003
misfit surface3.1L
Signal Reception and Detection: Sparse Arrays
GA Infrasonic Processing for CTBT monitoring
October 2003
equals
minus
Signal Reception and Detection: Sparse ArraysN
S
EW
N
S
W E
N
S
EW
GA Infrasonic Processing for CTBT monitoring
81 beams: 1.5 deg accuracy in azimuth
[BSSA, 2003, Vol 93 p.1765-1772]
October 2003
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• Determine the Great-circle intersection point
• Determine the travel-times to receivers using a two-value constant velocity model :
290 m/s (stratospheric propagation)240 m/s (thermospheric propagation)
• Determine if predicted travel-times match observed arrival times for both stations (up to some variance)
• Use uncertainty in measured azimuth to determine uncertainty in predicted source location
GA Infrasonic Processing for CTBT monitoring
detectionINFRA_LOC_0
automatic 2 station source location
origin
INFRA_LOC_1automatic
source location(refinement level 1)
INFRA_LOC_2automatic
source location(refinement level 2)
Network processing: Infrasonic source location
> 2 stations
Updated travel-timeInformation. GT information for testingData Fusion
origin
origin
October 2003
29
Summary
The Woomera Infrasound and Seismic experimento Characterised by unusually fast travel-times
• May be timing errors (unlikely)o Characterised by significant off-great circle azimuths
• may be side-lobe detections (unlikely)o May be acoustic signal generated by the seismic interaction with the Flinders
Ranges (?)
GA Infrasonic Processingo Seeks significant signals on individual stations first
• Basic set of discrimination criteria for automatic alert notification− Duration, Coherence, Energy
o Performs 2-station source location using constant velocity modelo Will experiment with the Kennett procedure for sparse array processing
• May help the spatial aliasing problem at sparse arrays