inertiallabs ins f1690039 post-processing report … raw data: inerdate2.trs post-processing results...
TRANSCRIPT
INS-T-306
Tersus GNSS-Aided Inertial
Navigation Systems
Test Report Version 1.0-20170516
Testdata:April 24,2017
Device:INS-T-306
Serialnumber:F1690039
INS-Tperformance:
• GNSS:Singleantenna,GPSL1/L2,GLONASS,20Hzpositions,20Hzmeasurements,• IMU: 200 Hz IMU measurements, 1 deg/hr gyro Bias in-run stability, 5 micro g
accelerometersBiasin-runstability
Flyingplatform:UAV(quadrocopter)
Project:airbornescannercarryingplatform(survey)
UsedPPsoftware:NovatelInertialExplorer
Testfiles:
INSdata:INERDATE1.Trs
Basestationdata:BaseStation_170125_XXXXX
GNSSrawdata:INERDATE2.Trs
Post-processingresults
SmoothedTCCombined-Map
Fig1.1
Estimatedpost-processedpositionaccuracyinwholetesttimeisshowninTable1.1andFig1.2.
Table1.1.Estimatedpositionaccuracy
East,m North,m Height,mSTD 0.0008 0.0008 0.0015RMS 0.0041 0.0046 0.0077Mean 0.0041 0.0045 0.0076
Fig1.2
Estimatedpost-processedattitudeaccuracyisshowninTable1.2andFig1.3.
Table1.2.Estimatedattitudeaccuracy
Heading,arcmin Pitch,arcmin Roll,arcminSTD 0.182 0.029 0.022RMS 1.990 0.293 0.289Mean 1.982 0.292 0.289
Fig1.3
Estimatedpost-processedvelocityaccuracyisshowninTable1.3andFig1.4.
Table1.3Estimatedvelocityaccuracy
East,m/s North,m/s Height,m/sSTD 0.002 0.002 0.001RMS 0.006 0.007 0.005Mean 0.006 0.006 0.005
Fig1.4
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