Seite - 124 - in Contributions to GRACE Gravity Field Recovery - Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
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Taylor point for the dependent observations ldep,0 completely cancels from eq. (9.1.29).
In the equation for the reduced derived observations, the term concerning the inde-
pendent observations can be considered as a correction term for the reduced dependent
observations, or
∆∆ldep=Find∆lind . (9.1.30)
With eqs. (9.1.22), (9.1.24) and (9.1.29) the right-hand side of the normal equation
system is
nR=A
T (
Σdep−FindΣTcro−ΣcroFTind+FindΣindFTind )−1( ∆ldep−Find∆lind )
.
(9.1.31)
9.1.2 Total Least Squares as Gauß-Markov Model with Eliminated
Observations
In this section, a different formulation for the treatment of uncertainties in the depen-
dent variables is proposed. Where Reinking, 2008 started from an extended observation
vector (eq. (9.1.5)), this formulation, perhaps equivalently, will begin with introducing
the independent variables into an extended parameter vector
ξ= [
x
lind ]
. (9.1.32)
This formulation pursues the goal of not only estimating the adjusted parameters xˆ
and the adjusted dependent variable lˆdep, but to also determine a least squares estimate
for the independent variable lˆind. The functional model eq. (9.1.1) is extended with a
second relationship describing the observations of the independent variable
ldep=f (lind,x)+edep (9.1.33)
lind=g(lind)+eind . (9.1.34)
This second relationship is of course simply
g(lind)= lind . (9.1.35)
This results in an extended observation vector identical to that of Reinking,
l= [
ldep
lind ]
. (9.1.36)
Linearising eqs. (9.1.33) and (9.1.34) at the Taylor point of the approximate values for
the parameters and the independent variable yields
ldep=f (lind,0,x0)+ ∂f
∂x ∣∣∣∣
x0,lind,0 ∆x+ ∂f
∂lind ∣∣∣∣
x0,lind,0 ∆lind+edep , (9.1.37)
lind=g(lind,0) + ∂g
∂x ∣∣∣∣
x0,lind,0 ∆x+ ∂g
∂lind ∣∣∣∣
x0,lind,0 ∆lind+eind . (9.1.38)
Chapter9 Co-Estimation of Orientation
Parameters124
Contributions to GRACE Gravity Field Recovery
Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Titel
- Contributions to GRACE Gravity Field Recovery
- Untertitel
- Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Autor
- Matthias Ellmerr
- Verlag
- Verlag der Technischen Universität Graz
- Ort
- Graz
- Datum
- 2018
- Sprache
- englisch
- Lizenz
- CC BY 4.0
- ISBN
- 978-3-85125-646-8
- Abmessungen
- 21.0 x 29.7 cm
- Seiten
- 185
- Schlagwörter
- Geodäsie, Gravitation, Geodesy, Physics, Physik
- Kategorien
- Naturwissenschaften Physik
- Technik