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GTK-R15

The GTK (Shenzhen) Technology Co., Ltd. GTK-R15 is a VTOL fixed-wing UAV optically pumped aeromagnetic system for airborne geophysical surveys. Integrated with the CW-15 platform, it combines rubidium and fluxgate magnetometry, navigation, altitude and attitude sensors, multichannel data acquisition, and software for magnetic compensation and survey-data processing.

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Product overview

Built for airborne geophysical surveying, the GTK-R15 combines a MEMS-based chip-scale rubidium atomic optically pumped magnetometer with a three-component fluxgate magnetometer, GPS, a laser altimeter, a nine-axis attitude sensor and a barometric altimeter. Hardware and software communications are integrated with the CW-15 flight platform. The system includes a miniature multichannel acquisition unit with a 24-bit high-speed ADC, a quad-core ARM Cortex-A53 processor running at 1.2GHz and USB data storage. Its navigation receiver supports GPS and BeiDou with 2m accuracy.

Windows ground-station software provides aeromagnetic data recording, post-flight cleaning, analysis and compensation parameter calculation. The optically pumped magnetometer compensation algorithm uses three vector components as attitude factors to remove aircraft permanent, induced and eddy-current magnetic fields from the total field. Its 18 coefficients are estimated from preliminary four-sided flight data collected in a magnetically smooth area as far above the ground as possible. The stored coefficients are then applied to data collected during subsequent survey flights. Fluxgate processing uses 12-parameter digital compensation.

The typical total-field interference improvement ratio is 10-20 times, varying with the flight platform and decreasing in systems with less interference. The optically pumped magnetometer operates from -30°C to +60°C and requires no calibration. At 5V, its probe and frequency counter consume 2 W during operation and 3W at startup. The probe measures 19x19x47 mm and weighs 18 g; the frequency counter weighs 100g, with connecting cables excluded from both weight figures. The fluxgate magnetometer has a ±100μT measurement range and a 15-minute warm-up time.

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Specifications

GTK-R15 specifications
SpecificationValue & conditions
Manufacturer, model and product typeGTK (Shenzhen) Technology Co., Ltd. GTK-R15 VTOL fixed-wing UAV optically pumped aeromagnetic system
Optically pumped magnetometer ground static noise0.01 nTFourth-order difference method; national aeromagnetic Grade 1.
Optically pumped magnetometer resolution0.0001nT
Optically pumped magnetometer measurement dead zoneSingle equatorial plane, ±7 degrees
Optically pumped magnetometer measurement range1000 nT - 100000 nT
Optically pumped magnetometer power supply and consumption5V; 2 W operating, 3W at startupProbe and frequency counter; operating and startup power.
Optically pumped magnetometer operating temperature-30°C to +60°C
Optically pumped magnetometer calibrationNot required
Optically pumped magnetometer maximum gradient tolerance100 nT/cm
Optically pumped magnetometer component weightsProbe: 18 g; frequency counter: 100gConnecting cables excluded from weight.
Optically pumped magnetometer probe dimensions19x19x47 mmProbe only.
Fluxgate magnetometer axes3Right-handed XYZ coordinate system.
Fluxgate magnetometer measurement range±100μT
Fluxgate magnetometer warm-up time15 minutes
Fluxgate magnetometer offset error±100nTIn zero field.
Fluxgate magnetometer scale error±0.5%DC.
Fluxgate magnetometer offset temperature coefficient1nT/°C
Fluxgate magnetometer orthogonality errorLess than 1°Between axes.
Fluxgate magnetometer digital output static noiseLess than 0.2 nT5Hz.
Fluxgate magnetometer digital sampling rate10Hz-1Hz
Acceleration and angular velocity resolutionAcceleration: 6.1e-5g; angular velocity: 7.6e-3°/sNine-axis accelerometer and gyroscope attitude measurement module.
Acceleration and angular velocity stabilityAcceleration: 0.01g; angular velocity: 0.05°/sNine-axis accelerometer and gyroscope attitude measurement module.
Attitude measurement stability0.01°Nine-axis accelerometer and gyroscope attitude measurement module.
Interference improvement ratio10-20 timesTypical total-field result; varies with flight platform, with lower improvement ratios in systems having less interference.
Optically pumped magnetometer sensitivity0.02nT /√Hz0.1-100 Hz frequency band; power spectrum.
Fluxgate magnetometer internal noiseLess than 10pTrms/√HzAt 1Hz.
Data acquisition hardwareMiniature multichannel data acquisition unit with 24-bit high-speed ADC, quad-core ARM Cortex-A53, 1.2GHz CPU and USB data storage
Navigation receiver2m accuracy; supports GPS and BeiDou navigation satellites
Sensor and platform integrationMEMS-based chip-scale rubidium atomic optically pumped magnetometer integrated with a three-component fluxgate magnetometer, GPS, laser altimeter, nine-axis attitude sensor and barometric altimeter; software communications and hardware integrated with CW-15; real-time or post-flight magnetic interference compensationIntegrated with the CW-15 flight platform.
Processing and compensation softwareWindows aeromagnetic recording and processing software with post-flight data cleaning, analysis and compensation parameter calculation; 12-parameter fluxgate digital compensation and 18-coefficient optically pumped magnetometer compensation using three vector components as attitude factors to remove aircraft permanent, induced and eddy-current magnetic fields from the total fieldWindows ground station; optically pumped compensation coefficients are estimated from preliminary four-sided flight data in a magnetically smooth area as far above the ground as possible, then stored and applied during subsequent survey flights.

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