4.4 the transient electromagnetic method (tem) · 4.4 the transient electromagnetic method (tem) 67...

4.4 The transient electromagnetic method (TEM)

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4.4.1 Basic principles and measuring techniques in TEM

By the transient electromagnetic method, TEM, the electrical resistivity of the underground layers down to a depth of several hundred meters can be measured. Groundbased measurements as well as airborne surveys (SkyTEM) to cover large areas are possible. The method was originally designed for mineral investigations. Over the last two decades the TEM method has become increasingly popular for hydrogeological purposes as well as general geological mapping. The electromagnetic geophysical methods are all based upon the fact that a magnetic field varies in time – the primary field – and thus, according to the Maxwell equations, induces an electrical current in the surroundings – e.g. the ground which is a conductor. The associated electrical and magnetic fields are called the secondary fields. Measuring technique

The TEM method applies an ungrounded loop as transmitter coil. The current in the coil is abruptly turned off, and the rate of change of the secondary field due to the induced eddy currents in the ground is measured in the receiver coil, usually an induction coil. The primary field is therefore absent while measuring. Figure 4.4.1 summarizes the basic nomenclature and principles. Typical measuring parameters for a groundbased system are: 1 – 20 ms on-time, 1 – 30 μs turn-off ramp and 1 – 20 ms off-time for measuring. The depicted waveform is often referred to as a square waveform. Other waveforms with sine or triangular shapes are used, but mainly in airborne systems.

Fig. 4.4.1: Basic nomenclature and principles of the TEM method. (a) Shows the current in the transmitter loop. (b) Is the induced electromotive force in the ground, and (c) is the secondary magnetic field measured in the receiver coil. For the graphs of the induced electromotive force and the secondary magnetic field, it is assumed, that the receiver coil is located in the centre of the transmitter loop.

The datasets are recorded in decay-time-windows, often called gates. The gates are arranged with a logarithmically increasing width to improve the signal/noise (S/N) ratio especially at late-times. This recording principle is called log-gating and 8–10 gates per decade in decay-time are commonly used. As shown in Figure 4.4.1, the current polarities in the transmitter coil and hence the primary magnetic field alternates for each single pulse. A typical sounding consists of 1,000 – 10,000 repeated single pulses (transients). The sign changes in the primary magnetic field are applied for suppression of: 1) the coherent noise signals from power lines, if the repetition frequency is chosen as a sub harmonics of the power line frequency and 2) offsets of the instrumental amplifiers. This measuring technique is referred to as synchronous detection. Field procedures

When performing fieldwork, a transient electromagnetic sounding can be conducted by placing a wire in a square loop on the ground as the transmitter coil, Tx-coil. When investigating the upper 150 m of the ground, a square loop

KURT I. SØRENSEN, ANDERS VEST CHRISTIANSEN & ESBEN AUKEN

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with an area of 40 x 40 m2 is commonly used. The receiver coil, Rx-coil, with a diameter of approximately 1 m is placed in the centre of the transmitter coil. The TEM principle

The measurements are carried out by ejecting a current in the Tx-loop. This results in a static primary magnetic field. The current is turned off abruptly and the related change in the primary magnetic field induces an electromotive force in the conducting surroundings. In the ground, this electrical field will result in a current which again will result in a magnetic field, the secondary field. Just after the transmitter is switched off, the secondary magnetic field from the current in the ground will be equivalent to the primary magnetic field (which is no longer there). As time passes by, the resistance in the ground will still weaken the current (converted to heat), and the current density maximum will eventually move outwards and downwards, leaving the current density still weaker. The decaying secondary magnetic field is vertical in the middle of the Tx-loop (at least if the ground consists in plane and parallel layers). Hereby an electromotive force is induced in the Rx-coil. This signal is measured as a function of time. Just after the current in the Tx-loop is turned off, the current in the ground will be close to the surface, and the measured signal reflects primarily the resistivity of the top layers. At later decay-times the current has diffused deeper into the ground, and the measured signal then contains information about the resistivity of the deeper layers. Measuring the current in the Rx-coil will therefore give information about the resistivity as a function of depth. The configurations shown in Figure 4.4.2 have the receiver coil placed in the centre of the Tx-coil and is called a central loop or an in-loop configuration. The receiver coil can be placed outside the Tx-loop which results in an offset-loop configuration.

Fig. 4.4.2: Field setup of a TEM system: a) Shows a central loop configuration, b) an offset-loop configuration. Rx denotes the receiver, Tx the transmitter, l the side length of the loop and h the offset between Tx-coil and Rx-coil centres.

4.4.2 Data curves

The decaying secondary magnetic field is referred to as b or the step response. However, because an induction coil is used for measurements of the magnetic field, the actual measurement is that of db/dt, the impulse response (the induced electromotive force is proportional to the time derivative of the magnetic flux passing the coil). The impulse response, db/dt is plotted in Figure 4.4.3 for a variety of halfspace resistivities.

Fig. 4.4.3: In a) the impulse responses (db/dt) for a homogeneous halfspace with varying resistivities are presented (black lines). The same curves converted to ρa are shown in b). The grey line is the response of a two-layer earth with 100 Ωm in layer 1 and 10 Ωm in layer 2. Layer 1 is 40 m thick.


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Figure 4.4.3 indicates power function dependence at late-times. At late-times, the impulse response can be written as

2521

2250

23z t

π20aμσI

tb --

≈∂∂

(4.4.1)

As seen db/dt has a decay development proportional to t-5/2. Observation of the decaying magnetic field in Figure 4.4.3 is not very informative and the same applies for actually measured sounding curves. A plot of apparent resistivity, ρa, is more illustrative. It is derived from the late-time approximation of the impulse response

3531

3502/1

z

2

a tπμ

)t∂b20

Ia(=ρ -

∂ (4.4.2)

The response curves plotted in Figure 4.4.3a are shown as ρa-converted curves in Figure 4.4.3b. The ρa-converted curves can be used as a data quality tool and as first estimate of the resistivity levels of the underground structure. 4.4.3 Background noise

A geophysical datum always consists of two numbers – the measurement itself and the uncertainty of the measurement. One single transient is affected significantly by the electromagnetic background noise. By repeating and stacking the measurement the background noise is decreased and the signal enhanced. Generally, a TEM sounding may consists of 1,000 to 10,000 single transients. Figure 4.4.4 shows stacks of 50 single transients and a stack of 5,000 single transients. It is obvious that a sounding with 5,000 stacked transients has a much better signal-to-noise ratio, S/N ratio, compared to the stack with 50 transients.

Fig. 4.4.4: TEM sounding curves stacked with 50 transients (grey) and 5,000 transients (black).

The electromagnetic background noise originates from various sources. Most sources, such as lightnings, are very distant. The fields from these sources travel around the globe in the wave guide cavity between the surface of the Earth and the ionosphere. This noise has a random character, and it is more powerful during the day than during the night and stronger during summer compared to winter. Background noise also originates from the power supply and the related man-made electrical installations. There are partly the 50 or 60 Hz signals and its harmonics, which have a deterministic character, partly the transient fields, which are of a random character and related to current changes in the power lines, when various installations are turned on or off. The deterministic part of the background noise from the power supply is removed by synchronous detection techniques, as mentioned before.


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With well-designed equipment the noise contribution from the electronics in the instrument itself is negligible compared to the noise contributions described above. It can be shown that using the log-gating technique, random noise contributions are decreasing proportional to t-1/2. It is evident that the signal level of measurements at early-times in most cases is many times larger than the noise level. This implies that the S/N ratio is high, and the uncertainty of the measurements is low at early-times. At later decay-times the decay signal is proportional to t-5/2. As the random noise level is proportional to t-1/2 it implies that the transition from a good S/N ratio to a poor S/N ratio happens quite suddenly. There are two ways to obtain datasets of a satisfactory S/N ratio at later decay-times, i.e. information from larger depths: 1) reduce the noise by increasing stack size or 2) increase the transmitted moment. Stacking reduces the noise proportional to N where N is the number of measurements in the stack. The effect of increasing the moment is shown in Figure 4.4.5 with the black dotted line. The line indicates the level of a sounding at the same location with a ten times larger moment and it is clear that the S/N ratio is much higher at later decay-times increased by a factor of ten. 4.4.4 Penetration depth

In relation to TEM soundings it is difficult, as for all other geophysical methods, to speak quantitatively and unambiguously about the penetration depth. In the following we will state some rules of thumb. The depth down to which the current system has diffused is called the diffusion depth. This depth, zd, is defined by

[ ] [ ] [ ]sμt,mΩρ,mtρ×26.1μσ

t2=zd ≈

(4.4.3)

Fig. 4.4.5: TEM sounding and noise measurements. The grey curves are noise measurements with the t-1/2 trend plotted with the thick dashed grey line. Error bars are 5%. The earth response is the black curves. The black dotted line indicates the approximate level of a sounding with a 10 times higher transmitter moment.

This is an exact equation for plane fields only. For circular or quadratic loop sources the diffusion depth is about 1.8 times smaller than estimated by Equation 4.4.3. As seen in the Figure 4.4.3, the signal decreases in a homogenous halfspace by t-5/2, and when the signal passes the level of the background noise, we can no longer use the measurements. Thus, the level of the background noise sets the limits for how late we can use our measurements. By using the expression given for dbz/dt for late-times we find a relationship between the noise signal, Vnoise, and the latest decay-time at which we can make measurements:


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)πσ

()V20M

(μ=t 5/35/2

noiseL

(4.4.4)

When tL is equivalent with the diffusion time td

)VσM

(551.0=)VσM

()π252

(=z 5/1

noise

5/1

noise

10/13d

(4.4.5)

From these expressions it is seen that the maximal diffusion depth, which is a measure for the penetration depth, is proportional to the fifth root of the ratio between the moment of the current loop and the product of the conductivity and the noise level. The only way to increase the penetration depth is to increase the moment of the transmitter or decrease the effective noise level, being the noise level after stacking and gating. The background noise is a relatively unchangeable size, but the way in which we gather and process our datasets, by stacking many measurements, reduces the effective noise. To double the penetration depth, the effective noise has to be reduced – or – the moment of the transmitter has to be increased by a factor 32. 4.4.5 Resolution and equivalence

The induced eddy currents are predominantly flowing in the good conducting formations. Therefore the resistivity and the layer boundaries of good conductors are very often well resolved. The eddy currents decay fast in high resistive layers and only weak measurable signals are produced. Hence in the presence of good conductors these signals often are neglectable and the resistivity level of high resistive formations is poorly resolved. In contrary, the layer boundaries may be resolved as these will coincidence with the boundaries of good conductors. The “geometry” of the high resistive formations may therefore be resolved. As mentioned before a geophysical measurement is described by its value and the uncertainty estimate on this value. Models that produce responses which compare to the measured

dataset within the estimated uncertainties are called equivalent models. Sometimes equivalences can be very pronounced in the sense that very different models give rise to almost identical responses. Equivalence appears in relation to thin good conductors embedded in resistive surrounding and vice versa. In these cases the resolution of the thin layers may be poor resolved. 4.4.6 Coupling to man-made installations

Distortion of datasets due to coupling to man-made electrical installations is not noise in the same sense as the random electromagnetic background noise described in the noise section. Coupling noise is a distortion and relates to induced currents in all man-made electrical conductors. The distortion has a deterministic character, arising at the same delay time for all decays and will therefore be summed in the stacking process. Coupling distortion in datasets cannot be accurately removed to provide a reliable interpretation; therefore soundings located close to man-made installations such as pipelines, cables, power lines, rails, auto guards and metal fences cannot be interpreted, and the dataset should be culled. The safe distance, defined as the minimum distance where undistorted datasets can be measured, is counted as the distance between any point on the transmitter-receiver setup and the man-made conductor. The safe distance to any man-made conductor is at least 100 m over an earth with an overall resistivity of 40 – 60 Ωm. The safe distance increases with the resistivity. 4.4.7 Modelling and interpretation

Data acquisition

As mentioned in the introduction, a main issue in applying the TEM method for hydrogeological studies is the demand for accurate and undisturbed datasets with high spatial density. Insufficient data quality makes it impossible to obtain a reliable geophysical model for use in a hydrogeological context.


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An important element of the data quality is the precise knowledge of the parameters of the applied instrument. To obtain datasets of sufficient quality, the following instrumental parameters must be known and modelled in the data modelling algorithm: The transmitted waveform characteristics,

including the exact appearance of the current turn-off and turn-on ramps and the timing between the transmitter and the receiver actions. Timing parameters must be known to an accuracy of 100 – 200 nanoseconds, because of their severe impact on early-time data.

The receiver transfer function, which is modelled by one or more low-pass filters, often has a strong influence on early-time data. Low-pass filters are implemented in the receiver system to stabilize the amplifiers and to suppress the noise from long-wave radio transmitters.

The geometry of the transmitter-receiver configuration must be accurate, especially for the offset-loop configuration. Central-loop datasets are relatively insensitive to deviations in geometry as long as the transmitter area is unchanged.

Measuring datasets with a high spatial density serves two purposes: 1) the resolution of geological structures is improved and 2) distorted datasets caused by instrument malfunction and transmitter-induced coupling to man-made conductors can be revealed and eliminated. The latter is by far the most important. Configurations, advantages and drawbacks

Ground-based TEM systems using a high transmitter moment normally utilize a transmitter loop of 40 – 100 m. The advantages of a large loop are that measurements can be carried out at the centre of the loop, and that the magnetic moment is large. The drawbacks are the low field efficiency and the higher possibility of coupling with man-made installations. A small transmitter coil with a high current is very field efficient, but four issues must be tackled in the configuration design:

Measuring in the central-loop configuration with a small transmitter coil and high output current may saturate the receiver amplifiers due to high voltages arising from the turn-off of the primary field. After saturation, amplifiers will produce distorted signals for several milliseconds. Furthermore, currents of the order of nanoamperes will leak in the transmitter coil after the current is turned off, adding to the earth's response and thereby to the distortion of the datasets. Both effects become negligible because of geometry when using either a small output current with a large transmitter loop or a large offset between the transmitter and the receiver coils. Thus high-output current datasets using a small transmitter coil must be measured in the offset-loop configuration, while low current datasets can be measured in the central-loop configuration.

The induced polarization (IP) effect is present in datasets measured in some sedimentary environments. The IP effect is most pronounced in datasets from the central-loop configuration, but moves to later decay-times when increasing the transmitter coil size. In offset configurations the IP effect is less pronounced and moves to later decay-times as the offset between the transmitter and the receiver coil is increased.

At early times, measurements using the offset configuration are extremely sensitive to small variations in the resistivity in the near surface. Extensive 3D modelling of such variations shows a pronounced influence on the measured datasets as the current system passes beneath the receiver coil. In many cases these datasets are not interpretable with a 1D model, even if the section is predominantly 1D. At later times, after the current system has passed, the distorting influence has decayed. Datasets from the central-loop configuration are much less affected by near-surface resistivity variations.

Datasets from the offset configuration are sensitive to small deviations in the array geometry. As an example assuming a 60 Ωm half-space model, a 30% error in the decay signal is apparent near the sign change if the receiver coil is located 71 m instead of 70 m


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from the transmitter. In a routine field situation, it is next to impossible to work with such accuracy. After the sign change, datasets from the offset configuration is essentially equivalent to that of a central-loop configuration.

A compromise is to use a high-power system with small transmitter loop, where early-time data are measured in the central loop configuration with a small current of 1 – 3 A. Late-time data are, in turn, measured in the offset configuration with maximum output current. In this way the four issues are addressed, and the field productivity can still be kept high. The 1D model

To this day it is not possible to invert TEM datasets in more than one dimension on a routine basis. 3D inversion codes have been developed lately, but they are still compu-tationally very demanding, and require densely measured datasets in at least two dimensions. Therefore, it is inevitable that geological noise, i.e. insufficient model presentation of the actual structure, is present when describing a 3D structure by a 1D model. The distribution of 2D and 3D structures decides the amount of geological noise. 4.4.8 Airborne TEM

Below we will present an overview of the requirements to airborne EM systems, especially TEM, and discuss the specific topics where the airborne and the ground based techniques differ. We will focus on the relatively new helicopter system, SkyTEM, as it provides the sufficient accuracy necessary for groundwater investigations. Hence the following comment on the main issues for airborne TEM is related to the application of the SkyTEM method. Special considerations for airborne electromagnetic measurements

In groundwater exploration, high quality data are required as the decisive data changes can be as low as 10 – 15 %. When operating airborne a

number of key issues need to be addressed to achieve this high data quality. The issues are mainly related to calibration, altitude and the flight speed. Calibration

In the context of requiring high data quality, the calibration of the transmitter/receiver system plays a central role. When airborne systems operate in the frequency domain, the strong primary field has to be compensated in order to be able to measure the Earth response. Because of drift in the system the compensation changes in time, and its value has to be determined successively during the survey by high-altitude measurements. Furthermore, it is necessary to perform measurements along tie lines perpendicular to the flight lines and by post-processing to provide concordance between adjacent lines. This process is called levelling, and because of this a frequency domain system is said to be relatively calibrated. When airborne systems are operating in the time domain, it is possible to reduce the interaction between the transmitter and the receiver system to a level, at which the distortion of the measured off-time signals is negligible. In this case, a calibration of the instrumentation can be performed in the laboratory and/or at a testsite before carrying out the surveys. Neither high altitude measurements nor performing tie lines for levelling are then necessary during the survey. Such a system is said to be absolute calibrated. The SkyTEM system has these capacities. The relatively calibrated systems will have a lower S/N ratio and lower data accuracy because of the drift and the levelling of datasets compared to that of absolutely calibrated systems. Altitude

For all EM airborne systems the Earth response decreases with increasing altitude. The random noise contribution from natural and man-made sources show no significant decrease within the operating altitude range compared to


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ground based measurements. Therefore, a higher operating altitude implies a lower S/N ratio at late-times, where the noise becomes predominant, and results in a poorer resolution of the deeper part of the Earth. The resolution of the near-surface layers decreases with increasing altitude because the induced eddy current system at early-times becomes larger and more spatial averaged. In general, increasing altitude means a lower resolution of upper layers. Another implication of the decaying Earth response with altitudes is increased distortions of the Earth response due to coupling to man-made installations. As mentioned before, a safety distance to installations of at least 100 m, depending on the subsurface structures, has to be maintained in order to avoid distorted datasets. Application of airborne electromagnetic measurements introduces larger safety distances to installations compared to ground based equipment, because Earth responses decreases with increasing altitude, whereas coupling responses in the operation altitudes maintain their signal level. The larger the operating altitude is the larger are the safety distances. Flight speed

An important tool for increasing the S/N ratio in electromagnetic measurements is to perform stacking of the measurements. In TEM measurements the background noise is reduced by stacking the transients. To achieve a required S/N ratio, a certain number of transients are necessary in the stack. When the system is moving while measuring, a trade-off exists between the lateral and the vertical resolution of the Earth parameters because a flight velocity related time interval is needed to collect the transients for the required stack size. The vertical resolution is related to the S/N ratio determined by the stack size. A certain stack size corresponds to a defined acquisition time interval.

The lateral movement while achieving the required stack size increases with velocity which implies a decrease in the lateral resolution. Hence, a higher vertical resolution inevitably means a decreased lateral resolution if the fight speed is unchanged. On the contrary, the same lateral resolution at a higher velocity results in a decrease of the S/N ratio and hence the vertical resolution. Data quality and post-processing

Airborne electromagnetic surveys are very cost effective. As the data acquisition is extremely fast, and large amounts of datasets are collected over a short period of time, the data quality control has to be automatic. As discussed before, the application of an absolutely calibrated TEM system, as the SkyTEM system, implies that no high-altitude measurements have to be carried out during the survey and subsequently used for compensating the datasets for the effects from transmitter-receiver interactions. Nor is it necessary to perform levelling of the datasets. In order to maintain the high data quality demanded for groundwater surveys, the geometrical setup of the equipment has to be well determined at all times, as well as the transmitted current waveform. The geometrical setup is determined by the altitude and the inclination of the transmitter and receiver coils. Furthermore, it is essential that the calibration and the functionality of the instruments are well documented, and that all setup parameters are saved for the subsequent interpretation. The post-processing of the measured datasets relates to two tasks. The first task is to process the altitude, inclination and position data in order to remove outliers and to provide continuity. Especially the altitude data need processing as they are, in many cases, affected by the vegetation on the surface. If the altimeter reflections from vegetation are not identified and corrected, errors will be introduced in the interpreted models. Figure 4.4.6 shows a section of altimeter data from the SkyTEM system. The dots are reflections as picked up by one of the laser altimeters mounted on the transmitter


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frame. The solid line is the processed altimeter data. The effects of the erroneous reflections obtained over the forest are removed in the processed altitude curve. Data from the processed altimeter data are used in the interpretation of the datasets.

Fig. 4.4.6: Processing of altitude data. Dots are the actual reflections picked up by a laser altimeter. The solid line is the processed height data. Over the forest a large number of reflections come from the tree-tops.

The measured inclination of the frame is used both to correct the altitudes and the datasets. Altitudes are measured assuming that the laser beam is normal to the ground surface. When the laser tilts, the normal altitude has to be calculated. The data compensation arises because it is assumed that the transmitter and the receiver are z-directed. This is not true when the frame is tilted. The second task is related to the distorting of the datasets by the coupling responses from man-made installations. This is a very time consuming process when operating in culturally developed countryside and involves a significant part of the post-processing time. However, the removal of coupling-distorted datasets is crucial for the quality of the interpreted datasets. Figure 4.4.7 is an example from a SkyTEM survey where the survey line crosses two couplings associated with roads. The data marked with grey in Figure 4.4.7a are coupled, and like the sounding curve in Figure 4.4.7c they can not be used for interpretation. The uncoupled data in Figure 4.4.7b have a smooth appearance in the whole time range until they reach the noise level for the last couple of gates.

Fig. 4.4.7: Coupled datasets. Panel a) is a plot of selected time gates along a profile from a SkyTEM survey. Data are normalized with the transmitter moment. Datasets marked with grey are identified as coupled whereas black data are uncoupled. The coupled datasets are associated with the crossing of two roads. Plot b) shows a coupled dataset, and for comparison an uncoupled dataset is shown in c). Profile and position of selected soundings are shown on the inserted map in d). The coupled sounding is marked with a circle, the uncoupled sounding with a square. The thick solid line marks the profile section shown in a).

4.4.9 The SkyTEM system

The SkyTEM system has been developed for groundwater investigations by the HGG group at the University of Aarhus, Denmark. During the last 4 years, the system has been intensively used for groundwater surveys. A key issue for the system development was that the measured datasets present the same quality as those from the groundbased TEM systems. The transmitter and receiver coils, power supplies, laser altimeters, inclinometers, global positioning system (GPS), electronics, and data logger are carried as a sling load on the cargo hook of the helicopter. SkyTEM in operation is pictured in Figure 4.4.8.


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Fig. 4.4.8: The SkyTEM system in operation

The array is located using two GPS position devices. Altitude is measured using two laser altimeters mounted on the carrier frame, as well as inclinometers measuring the inclination of the carrier frame in both the x and the y directions. The measured datasets are averaged, reduced to data subsets (soundings) and stored together with GPS coordinates, altitude and inclination of the transmitter/receiver coils and transmitter waveform. Transmitter waveform information and other controlling parameters of the acquisition process are recorded for each data subset, thereby ensuring high data-quality control. The transmitter loop is a four-turn 300 – 500 m2 loop divided into segments to allowing transmittance of a low and a high moment. The transmitter loop is attached to the rigid Kevlar reinforced epoxy/wood composite lattice frame. The receiver coil is located on top of the rudder, 1.5 m above the corner of the transmitter loop as shown in Figure 4.4.8. The operational flying speed of the SkyTEM system in groundwater surveys is 20 – 40 km per

hour (5.5 – 11.0 m/s) providing a high-moment stack size of approximately 1000 transients. This is sufficient to obtain time gates out to 2 – 6 milliseconds. Consequently high- and low-moment dataset segments yield an average lateral spacing of 30 – 50 m. A compromise between vertical resolution and safety concerns for the helicopter operation is to maintain an altitude of 15 – 20 m for the carrier frame and about 50 m for the helicopter. In forest areas, the flying altitude increases with the height of the trees. The SkyTEM system is absolutely calibrated at the national test site in Denmark before used in surveys. Occasionally the systems are brought to the site to ensure that the equipment is operating correctly. As part of the standard field procedure for data quality check, repeated datasets are measured at a local testsite every time the helicopter refuels and gets fresh batteries, at about 1.5 – 3 hour intervals. The repeated measurements when corrected for the geometrical parameters (altitude, inclination etc.) are expected, generally, to be within 5%. Processing of SkyTEM data

Navigation and status data for the SkyTEM system make up a substantial amount of data. The basis for the processing is the following: GPS data are measured every second with

two independent devices.

The inclination of the frame is measured every second by two independent devices.

The altitude of the frame is measured 20 times per second with two laser devices.

The transmitter current is stored for every 50 – 100 transients. The transmitter also monitors parameters like battery voltage and temperature.

Every transient is stored and saved for further processing.


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Processing of GPS and inclination data is done by adaptive filtering of the datasets. The inclination data are used to calculate normal reflection altimeter data and for calculation of exact transmitter and receiver altitudes and a field correction factor. The field correction factor accounts for the reduction in the z-directed magnetic moment caused by the movements of the transmitter/receiver-plane when flown in the wind. The inclination from horizontal is normally between 0 and 15 degrees. Processing of the altitude data is more critical and has to be evaluated by the user. A precise determination of the altitude is crucial to obtain the required resolution of the upper approximately 30 m of the subsurface. The main problem is that the lasers receive reflections from the canopies and not the forest floor when the system flows over both hard-wood and soft-wood forests. This is seen as abrupt drops in the altitude measurements. An adaptive filtering scheme has been designed to eliminate the unwanted reflections, but also this scheme fails when forest-floor reflections are absent in tens of seconds. In this case, the user has either to draw an altitude line on a profile plot of the altitude data or, if impossible, to mark the altitude as a free parameter in the inversion. The processing of the transient datasets is done in two steps. The first step uses adaptive filters to eliminate noise. The stack size after step one is approximately 100 – 200 transients. At this stage,

all datasets that are coupled due to man-made installations are removed. This process is quite time consuming and requires a close integration of gate profile plot, individual dataset plots and a GIS-map. In step two, the datasets from step one are averaged into dataset sequences. The dataset sequences are the final soundings used in the inversion. A final sounding consists of about 600 – 800 SkyTEM transients yielding time gates from 12 µs to 2 to 6 ms. The soundings are on the average separated 30 – 50 m on the flight line. Inversion of SkyTEM data

A sounding consists of a low and a high-moment segment. As the two segments are spatially separated, the dataset sequences are inverted with different altitudes. The flying altitude is included as an inversion parameter with a prior value and a standard deviation determined from the altimeters. All dataset sequences along the profile lines are inverted in one step using soft bands on the model parameters. This approach allows for smooth transitions along the profile line resembling the actual changes in geology. SkyTEM was operated in a number of pilot areas of the BurVal project. Examples are shown, e.g., in Chapter 5.4 Ellerbeker Rinne.


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4.4 the transient electromagnetic method (tem) · 4.4 the transient electromagnetic method (tem) 67...

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