Field manuals

AEM

Airborne Electromagnetics

A transmitter loop slung beneath an aircraft induces currents in the ground and a receiver measures the secondary field in parts per million. It is the fastest way to map conductivity over large exploration areas.

Crew

Pilot, system operator, ground data QC geophysicist

Mobilisation

3-5 days: ferry, bird rigging, calibration flights, permits

Daily coverage

200-400 line-km per flying day

Equipment and specifications

PlatformHelicopter with 30-40 m tow, or fixed-wing with towed bird
TransmitterMulti-turn loop, 300 Hz - 200 kHz (frequency domain) or 25-30 Hz base (time domain)
ReceiverThree-component induction coils, in-phase and quadrature at each frequency
AltimetryRadar plus laser altimeter, 0.1 m resolution
NavigationDifferential GNSS, 1-2 m along-line positioning

Setup sequence

  1. 01

    Plan the flight

    Line spacing 2-4x target width, flown across strike, with tie lines every 10 lines.

  2. 02

    Calibrate

    High-altitude zero and calibration-coil checks at the start and end of every flight.

  3. 03

    Hold terrain clearance

    Nominal 30-40 m bird height; log every departure for later levelling.

  4. 04

    Monitor drift

    Watch the zero level in real time; return to a repeat line if drift exceeds spec.

  5. 05

    Level and grid

    Apply calibration, remove drift, level to tie lines, then grid each channel.

Safety

Low-level flight

Terrain clearance minima, obstacle survey, daylight VFR only.

Sling load and bird

Rigging checks, hook-up drill, exclusion zone under the aircraft.

Fatigue

Duty-time limits for pilot and operator, mandatory rest between sorties.

Fuel handling

Bonding, spill kit and no-smoking zone at the fuel cache.

Field vs lab

AspectIn the simulatorIn the field
Signal-to-noiseClean synthetic response; noise added only if you ask for it.Cultural noise, wind and instrument drift set the usable dynamic range.
Flight heightA fixed number you set once.Varies continuously with terrain; the single biggest amplitude control.
System driftNone.Thermal drift needs high-altitude zeros every 30-60 minutes.
CultureAbsent.Powerlines, fences and pipelines produce anomalies larger than the target.
RepeatabilityIdentical parameters return an identical curve every time.Coupling, moisture and temperature move the response between repeats.

Field QC checklist

  • · High-altitude zero drift within the system specification per flight
  • · Line separation within 20% of nominal for 95% of the block
  • · Tie-line misfit under 2 ppm after levelling