Three-Dimensional Absolute Orientation e)f Stereo Models Using
ABSTRACT: A method for using digital elevation models (OEMs) as exclusive information for absolute orientation of stereo models is investigated.
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Closed-form solution of absolute orientation using unit
Closed-form solution of absolute orientation using unit quaternions. Berthold K. P. Horn. Department of Electrical Engineering University of Hawaii at
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Closed-form solution of absolute orientation using unit quaternions
measurements is referred to as that of absolut e orientation The problem of absolute orientation is usually treated in a n.
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Closed-form solution of absolute orientation using orthonormal
Closed-form solution of absolute orientation using orthonormal matrices. Berthold K. P. Horn*. Department of Electrical Engineering University of Hawaii at
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Closed-form solution of absolute orientation using
Received June 2 1987; accepted March 251988 Finding the relationship between two coordinate systems by using pairs of measurements of the coordinates of a number of points in both systems is a classic photogrammetric task The solution has applications in stereophoto- grammetry and in robotics
People MIT CSAIL
This paper presents a closed form solution of absolute orientation using unit quaternions which is a fundamental problem in photogrammetry and computer vision The paper also discusses the properties and applications of quaternions and compares them with other rotation representations
Three-DimensionalAbsoluteOrientatione)f
StereoModelsUsingDigitalElevation
DanRosenholmandKenner!Torlegard
control whereX o,Yo,and2
0 aretranslations,misthescalefactor,and theorthonormalrotationmatrixisINTRODUCTION
T also fromFORMULATION
elevationofapointwithplanecoordinatesX,Y intheground themeasuredmodelcoordinates(x ij,YwZij)p,wherex,y,zare
mulation,theindiceswillnotfurtherbeused. as (2) (4) m+mJ+mRm r32=sin(t)cos(a)+cos(t)sin(T})sin(a) r 13 =sin(T}) r 23=-sin(t)cos(T}) r33=cos(t)cos(T}) respectively.Linearization aroundg=T}=a=I)andm=1,aspe tionsystemforabsoluteorientation:
Thisformulationdescribes
howdifferentialchangesinthe2+Ll2=2
0 +m(Y31x+Y32Y--Y33z) +Ll2 0 xLlT}+YA£+zLlm(3) coordinatesintheOEM:2=I(X,Y)Ll2=dlLlX+dlLlY
dX dY aroundg=T}=a=Oandm=1,LlX=dX
o +xdm-yda+zdT}LlY=dY
o +Xda+ydm-zdg(5) vation systems,i.e.,theOEMandthestereomodel:A=2 -2
0- m(Y 31x+Y 32
Y+'33z)
(1) m+mRmTherotationelementsareherechosentobe
r ll cos(T})cos(a) r 21cos(t)sin(a)+sin(t)sin( r31 sin(t)sin(;a)-cos(t)sin( r'2=---cos(T})sin(a) r22=cos(t)cos(a)-sin(t)sin(T})sin(a) d2 0- xdT}+Ydg+zdm -:{(dX o +xdm-yda+zdT}) -(dY o +xda+ydm-zdt) (6)
©1988AmericanSocietyforPhotogrammetry
andRemoteSensing vorable.This meansthateachpointinthisexampleshouldbe cerningslopeasindicatedinFigure1.THEINVESTIGATIONMETHODS
parativetest inStockholm, wheretheworkreportedinthispaperwasper formed.Threeof thesixareasusedinthecomparativetestwere ure (Figure4).Foreachtestarea threemodelsmeasuredbythe aspossible(given thenumbers''1''inthetables),onewith of polationin differenttest areasalsohaddifferentnumbersofgridpoints (Table1).Thecalculationsinthisinvestigation
wereperformedasabFIG..1.Anexampleofthenec
essaryelevationandslopein formation intheOEM. matevaluesofthetransformationareused. derivativesare thechangeinZintheOEMcorrespondingtoa thecomputationofthefirstderivatives. Thisisdonemainlyfor apractical derivativeswillgiveerrorsin thedesignmatrix.Thediscrete firstderivativein xisthusinthisinvestigationcomputedas (7) pendingontheactualOEMstructure. The6aresolvedfor
bytheleast-squaresmethod.Therotationpa untilconvergence.Aftereachiteration,all pointsinthestereo each tion tance,thescalefactorbyless than0.05percent,andtherotations astatisticaltestof thejointsignificanceoftheunknownsinthe adjustment. vationscanbe computedbyclassicalerrorpropagation.WHATSLOPEANDELEVATIONINFORMATIONARE
NEEDED?
orientation.InFigure1 thediscussionisillustrated.Inallseven thatwillbedeterminedisshownforeachpoint.First,
minationofdZ o.TherotationsaroundtheX-andtheY-axes(dg
three togetherwithatranslationinplane(saydY o ),determinedby directions.Thenexttranslationinplane(dX o) needsonefurther nally thez-axisimpossibleisneeded(da). slopes)are proximationsof therealslopes.Iftheslopeissmall,thenthe •dE jda jdm dX DApPROXIMATEMEANSLOPESINXandy.
#GridPointsGridAreaSizeSlope%
TestAreainx
inySpacinginxinyinxinyBohuslan643519.81m1248m674m6.3 6.6Stockholm
46 4511.98m539m527m5.67.4Siihnstetten
1042011.38m1172m216m14.525.7
gardedasgivencontrol).Asinitialvaluesnotranslations(X
o =Yo=2 0 ),norotations valuesisnotinvestigated.RESULTSANDDISCUSSION
ACOMPARISONTOTHERESULTSOFTHEISPRS-TEST
intheISPRS-test. thelevelingdoneintheISPRS-test. inthecomparativetestcorrespondsto2 0, and17,whileX o,FROMTHEISPRS-TESTAREGIV:N.
ThisInvestiga-
tionTheISPRS-test (RMS)InitialGrossE.
ComputationRMSlT
oInitialExclus.Level
Bohuslan11.320.83
1.311.30 1.03
Bohuslan21.621.48 1.62 1.50 1.43
Bohuslan32.442.18 2.35 2.252.15
Stockholm10.59 0.50 0.64 0.540.52
Stockholm21.290.951.32 1.25
1.11Stockholm33.19d)3.23 3.23 3.12
Siihnstetten1
0.380.210.380.380.24
Siihnstetten20.48
0.410.480.42 0.38
Siihnstetten31.221.15 1.19 1.101.08
XoYo2 01)aComputationmetremetre metremrnradmrad mrad
Bohuslan11.82.80.71.00170.6
-0.1-3.0Bohuslan20.2-2.80.30.99920.40.7-0.1
Bohuslan33.7-3.30.80.99770.11.02.5
Stockholm11.40.50.0
1.0021-0.50.7-3.0
Stockholm2-1.01.10.31.0169-0.1-0.3-10.9
Siihnstetten1-0.30.5-0.41.00070.3 0.8-0.7
Siihnstetten20.0-0.20.41.0025-0.1 -0.1-1.1
Siihnstetten3-0.10.7 0.00.9979-0.4 -1.9-0.5
investigationcomparedtotheISPRS-test.
parametersare shown. (redundancy)inthis study,allratiosbetweenthecomputed fact participantsinthetest. absoluteorientation, andabsoluteorientationwithOEMsisto comparethe propagatedstandarddeviationsoftheunknown of (,TJ,X o,Yo,and2
0 fromanabsoluteorientationinaKern andaccordingto the The operator.InTable6thecorresponding standarddeviationsfrom theabsoluteorientation withOEMsarepooledforeacharea.Absoluteorientation
withOEMsgivesahigherprecisionof thejointheightparameters (2 0,TJ,g).Thedifferenceishighly
significantconcerningthe2 0 parameter,whichinthiscase THEORIENTATIONWITHDEMs.
u Xo CY{U aComputationUometremetre metreU
m mradmrad mradBohusHin10.83 0.320.310.030.00090.20.11.0
BohusHin21.480.480.47 0.050.00120.20.11.3
BohusHin32.180.67 0.680.070.00170.30.22.0
Stockholm1
0.500.180.14 0.020.00080.10.10.8
S6hnstettentl0.210.04 0.05 0.020.00020.00.10.2
S6hnsteten20.410.07 0.09 0.040.00040.00.20.3
S6hnstetten31.150.200.26 0.100.00100.10.7 0.7
THE Uo uTIComputationmetre metre metre metremradmrad
Bohuslan0.70.6 0.4 0.80.270.31
Stockholm0.30.2 0.20.40.090.16
S6hnstetten0.10.1 0.1 0.10.060.10
DEVIATIONSOFTHE
SAMEABSOLUTEORIENTATIONPARAMETERSASIN
TABLE2AFTERABSOLUTEORIENTATIONWITHDEMS.
Uo CYxoo U Yo CY TIComputationmetremetremetremetremradmrad
Bohuslan1.600.510.510.050.20.1
Stockholm0.76 0.42 0.420.040.2 0.2
S6hnstetten0.720.120.160.060.10.4
is accuracyobtainedfromclassicalorientation oncontrolpoints.MODELFIDELITY
1986).
does theproblemsWehaveerrors
inthedesignmatrixbecauseoftworeasons. overaTheobservations(theright
handside)arealsoaffected.The interpolationsintheOEM,performedbetweeneachiteration,
are fromtheestimationmodel thatisveryimportant. In distances, investigation.CONCLUSIONS
andtheslopecharacteristicsoftheobject. In tional vation.Theaccuracyinplanimetryishighly dependentontheThetypeofterrain,
willinfluencetheaccuracyofthesolution. The regulargrids ineitherthegroundOEMorinthestereomodel derivatives andoftheinterpolationintheOEM. allybeapproximated bytheunitmatrix,makingthecompu tationsverysimple. The asa pho graphicinformationcan thusbeusedforabsolute orientation. redundancy. soluteorientation. errorsin1986b,1987)
ofphotogrammetryandforrobotvision.ACKNOWLEDGMENTS
forgivingusaccesstotheir resultsfrommeasurementsintheNewSustainingMember
Rosenholm.
REFERENCES
eralizedModel beiderErzeugungDigitalerGelandemodelle.InternationalArchives
ofRoyalInstituteofTechnology,Stockholm.
metry,Vol.XXVI,Comm.III,pp.573-587.621-626.
ModelsusingDigitalElevationModels.
ProceedingsoftheACSM
ASPRSAnnual
ConventionPart4,pp.241-250.
430.grammetria,Vol.41,No.1,pp.1-16. (Received
10June1988;accepted17June1988)
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