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ons that is
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(4)
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International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Vol XXXV, Part B3. Istanbul 2004
Own Pay Tur 9:
oO Oo oO
C. ou o m mme tous
A ET
0 O zx Oy O zz OzT
Or Og Or Orr
Where the diagonal elements of the matrix refer to the are
Oxx the variance of X, Cyy variance of y, OZ
variance of Z , and OrT variance of time, and off-diagonal
elements are covariances. Various dilutions of precision factors
can now be computed:
The horizontal dilution of precision is defined as:
IHDOP-- ——— ——— (10)
and the vertical dilution of precision as:
yDOP.s. -—Z. (11)
The semi-axis of the confidence regions are related to the
eigenvalues of this matrix (Vanicek, P. and E.J. Krakiwsky, ,
1986)
2. DATA COLLECTION AND VALIDATION
To practically verify the GPS error model, and estimate the
positional error of the measurements of ground control points
using a GPS code receiver, the discrepancies between receiver
coordinates and reference coordinates are computed in a study
area around the ITC building in Enschede, The Netherlands
using a Garmin map 76s code receiver and a Leica 300
differential carrier phase instrument. The coordinates of the
points obtained by carrier phase measurement were used as
reference, to compute errors of the code measurements.
3. COORDINATE SYSTEMS.
For the analysis 3 different coordinate systems were used:
-WGS 84, which is the common GPS coordinate system.
-RD and NAP, Dutch coordinate system, used in The
Netherlands.
- Local (plane tangential) system,
The transformation parameters used to transform data from
WGS84 to RD and NAP, used in phase observation, are
different to that applied by Garmin code receivers. Therefore
the geodetic WGS84 coordinate ( Q, À, h) is converted Ta X,
629
Y, Z geocentric coordinate, and discrepancies AX, AY, AZ are
computed.
To be interpretable for practical use, geocentric discrepancies
AX, AY, AZ are transformed into a plane tangent to the earth
surface, at the centre of gravity of the study area, the local
coordinate system (AN, AE, AH).
The following equations were applied for the transformation of
discrepancies from AX, AY, and AZ to the local coordinated
system in the plane surface, which is shown (AN, AE, AH)
AE =—AX -sinA+ AY - cosA
AN =—AX - cosÀ - sinp — AY - sind - sinp + AZ - cos (11)
AH = AX - cos - cos + AY - sind - cosp+ AZ - sing
Where, @ refers to the geodetic latitude of a target point and À,
is defined as the geodetic longitude of a target point.
4. RESULTS
The average of discrepancies p represents the deterministic
error, and c indicates the stochastic error. Four different
observation times (1, 3, 5 and 10 minutes) were used, applying
a Garmin map76s handheld receiver. The following tables show
the result in the local coordinate system.
Discrepancy | u | o | s | RMSE
AX -0.78 455 213 224
AY -1.04 5.67, 2382 2,56
Cov. -0.99
Correl. oeff. -0.19
Plani. MSE 3.40
Table 2. Statistics of Discrepancy of 1-minute observations:
Discrepancy u | c? | o | RMSE
AX -0.72 3.02 1.74 1.87
AY -l.04 5.14 227 2.48
Cov -0.96
Correl. coeff. -0.25
Plani. RMSE 3.11
Table 3. Statistics of Discrepancy of 3-minutes observations:
Discrepancy | u | c? | o | RMSE
AX -0.46 2.12 1.46 1.52
AY 0.82 5.60 2.38 2.32
Cox 0.17
Correl.coeff. -0.06
Table 4. Statistics of Discrepancy of 5-minutes observations