Non-destructive PCB/IC testing
NV magnetometry images current paths to find shorts & opens without probes.
Underground mapping
Cold-atom gravimeters locate voids/tunnels for civil engineering and geology.
GPS-denied navigation (MagNav)
Airborne magnetometers track Earth-field gradients to aid navigation; requires high sample rates with good sensitivity.
Decode the spec sheet
- Sensitivity (η) in T/√Hz — Sometimes referred to as noise density, the sensor’s noise floor per √bandwidth. A lower sensitivity is what everyone wants.
- Bandwidth (BW) The range of frequencies of the magnetic field that can be detected. Application specific.
- Coherence (T2*) How long the sensor can maintain its coherence-enhanced magnetic sensitivity. A higher coherence time lowers sensitivity
- Dynamic range The range in the strength of the magnetic field that can be detected. Application specific.
SNR vs time (play with it)
Model: for white noise, SNR grows as
SNR ≈ (Signal/η) · √(T/BW)
.
Here η is noise density in T/√Hz, BW is measurement bandwidth (Hz), and T is your averaging/integration time (s).
The minimum detectable field at SNR≈1 is
Bmin(T,BW) = η · √(BW/T)
.
Sensitivity 101: why T/√Hz matters (and MagNav)
T/√Hz is a convenient way to quote a sensor’s fundamental noise, and thus sensitivity. If you average for time T,
white noise falls as 1/√T. If you need higher sample rate (larger BW), noise rises as √BW.
That's why a longer measurement time results in the ability to detect smaller magnetic fields. An application that requires a high sampling rate will increase the minimum detectable magnetic field
(1×√(10/1)
), but only ~1 nT at 100 Hz BW — and much worse at 1 kHz.
MagNav implication: an aircraft moving quickly needs ≥100–1000 samples/s to resolve geologic/urban gradients without aliasing. This high requirement for the sampling rate often requires non-sequential vector readout. Practically: pick a magnetometer with the lowest η you can afford and validate Bmin(T,BW) at the mission’s sample rate to ensure you can detect the target signal.
What to measure in a pilot
- In-field noise density vs temperature and vibration
- Calibration drift over hours; re-zero procedure and time
- Packaging and alignment stability (optics, vacuum)