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1 Comparison of Ground Magnetic and Low Altitude Aeromagnetic Data R. S. Bell Geophysicist & geoDRONEologist September 29, 2017 SEG Near Surface Technical Section International Geophysical Service, LLC Tel: 303 - 462 - 1466 e - mail: [email protected] www.igsdenver.com SEG 2017 Annual Meeting Post-Conference Workshop Drones Applied to Geophysical Mapping

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  • 1

    Comparison of Ground Magnetic and

    Low Altitude Aeromagnetic Data

    R. S. BellGeophysicist & geoDRONEologist

    September 29, 2017

    SEG Near Surface Technical Section

    International Geophysical Service, LLCTel: 303-462-1466 e-mail: [email protected] www.igsdenver.com

    SEG 2017 Annual Meeting Post-Conference Workshop

    Drones Applied to Geophysical Mapping

    mailto:[email protected]

  • 2

    Objective

    Assess data fidelity as well as applicability

    of drone based magnetometry using a off-

    the-shelf small UAS and the prototype of

    the MFAM based MagArrow magnetometer

    made by Geometrics, Inc.

    Our “standard” were data ground magnetic

    survey data acquired using a Geometrics

    G-859 Cesium Magnetometer a.k.a. “the

    Mineral Mag”.

  • 3

    G-859 SpecificationsOperating Range: 20,000nT to 100,000nT

    Noise: 20,000nT/m

    Temperature Drift:

  • 4

    The MagArrow

    prototypeweight: 2.3 kg ( 5.1 lb)

    Power – 2.5 W per Sensor

    Weight – Less than 2 lbs.

    15 cm3 sensor elements

    Sample Rate – 1000 Hz.

    Sensitivity – 0.001 nT/√Hz

  • 5

    The sUAS Specifications

    Make / model: DJI Matrice 600 Pro

    UAV type: X-6 (hexacopter)

    MTOW: 34.2 lbs

    Lift capacity @ msl: 12.2 lbs

    Horizontal speed: 0 to 40 mph

    Operational ceiling: 14,750 feet

    Max wind speed resistance: 18 mph

  • 6

    The sUAS Specifications

    Make / model: DJI Matrice 600 Pro

    UAV type: X-6 (hexacopter)

    MTOW: 34.2 lbs

    Lift capacity @ msl: 12.2 lbs

    Horizontal speed: 0 to 40 mph

    Operational ceiling: 14,750 feet

    Max wind speed resistance: 18 mph

  • 7

    The sUAS Fly by Test

    ~1.1 nT

    ~2.1 nT

  • 8

    The sUAS start up noise test

    • The G-859 sensor was placed 1 meter from center of sUAS

    • Operator initiated start up and lift off sequence of aircraft

    • Once flight altitude was achieved he flew away from site

    Test sequence for

    camera gimbal

    lift off

    > 10 nT

  • 9

    Comparison of MFAM data with Ground Magnetometer Data

    Geometrics G-859

    Sensor 1 Sensor 2

    MFAM (MagArrowTM) GPS Line locations

    Data are raw total magnetic intensity (TMI) data. The

    data have not been corrected or leveled.

  • 10

    UAS Magnetometry Example – Landfill

    line separation: 10 m

    UAV altitude:

    Block 1 & 2: 15 m AGL

    Block 3: 20 m AGL

    MagArrow altitude:

    Block 1&2: 11.5 m AGL

    Block 3: 16.5 m AGLFlight Path

    superimposed

    on 1m DEM

    FB-1

    FB-2

    FB-3

    500 m

    50

    0 m

  • 11

    Observed Total Magnetic Intensity (TMI)

    3 flights x 15 minutes per flight

    Total time on site: 2.5 hours

  • 12

    RTP Total Magnetic Intensity

  • 13

    CVG of RTP Total Magnetic Intensity

  • 14

    CHG of RTP Total Magnetic Intensity

  • 15

    Ground Survey - Total Magnetic Intensity (raw)

    Sensor altitude: 2.3 m AGL

  • 16

    Total Magnetic Intensity (raw)

    Ground Survey

    UAS Survey

  • 17

    Summary & Conclusions

    ➢ The ground survey required 2 days to complete while

    the UAS survey was accomplished in 0.5 days.

    ➢ The UAS magnetic data compare very well with the

    ground magnetic data. No lag corrections were

    needed to geo-reference the airborne survey results.

    ➢ The UAS was test flown at a sensor altitude of 6.5

    meter AGL but the pilot was not comfortable with

    flying so low. Nevertheless, it was clear that one

    could safely fly a UAS survey such that the magnetic

    field sensor was at the altitudes typically used for

    ground survey.

  • 18