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Technical Notes - Helicopter Electromagnetics

What is that Noise on a DIGHEM/RESOLVE System?

What is noise, indeed? The internal electronic noise of a well-adjusted helicopter electromagnetic system is well below the numbers shown on the chart below - usually below 1 ppm. The noise levels shown here are "average" under field conditions, and may include sferics, power lines, vibrations, etc.

The second dimension to noise is the frequency content. These values are a rough measure of the shorter period (higher frequency) noise, from a few 10's of seconds to higher. This is the noise that is critical in the anomaly detection band, which is around 2 to 10 seconds. Any noise shorter than about 1 second is easily filtered because it doesn't affect any signal in which we are interested.

The critical noise for resistivity mapping is the very long period - normally called drift. The drift quoted in this table is the uncorrected drift between high altitude base level checks. This drift is greatly reduced by a linear interpolation between the values measured at the high altitude tests. The only remaining drift in the data given to the interpreter is the non-linear component of this drift. This last component is removed to less than 1ppm in the leveling and processing.

DIGHEM/RESOLVE STANDARD VALUES RMS

  RMS Chart Recorder Quoted Noise and Drift
FREQ   SEP'N   Chart   Clip Resol'n Drift 20 min Noise -flat Noise -rough
Hz
 
M
mV/ppm
ppm/cm
mV/cm
ppm
ppm
ppm
ppm
ppm

380

CP
7.98
2.5
50.0
125
4000
0.12
10
2.5
5
900
CP
7.98
2.5
50.0
125
4000
0.12
10
2.5
5
1000
CX
7.98
5
25.0
125
2000
0.06
10
4
8
5500
CX
7.98
2.5
50.0
125
4000
0.12
20
10
20
7200
CP
7.98
 1.25
100.0
125
8000
0.24
20
5
10
56k
CP
6.32
 0
200.0
100
20000
0.6
30
20
40

 

Greg Hodges, Chief Geophysicist, 2001


1Noise in EM data is usually considered by its period - the wavelength in time. High frequency noise has a short period. The smallest coaxial EM anomalies over discrete conductors have a period of about 5 seconds.

 

 

 
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Technical Notes