Page - 64 - 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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specific time lag. LetVn be the Nmax×Nmax identity matrix for n= 0, and a zero
matrixwithonlythe n-th lowerandupperdiagonalonesotherwise,e.g. for Nmax=5
V2= 






 0 0 1 0 0
0 0 0 1 0
1 0 0 0 1
0 1 0 0 0
0 0 1 0 0 






 . (6.5.16)
The cofactor matrix eq. (6.5.6) is then
Qmll= Nm−1
∑
n=0 Cnxx ·Vn . (6.5.17)
Each value of the discretised covariance function corresponds to one specific covariance
componentVn, and as such they can be separated using VCE. The arc-wise variance
factors, the variance factor determining the weight of one individual short arc of one
observation type w.r.t. all other arcs of that observation type, depend on the sum of all
individual cofactor matrices associated with all time lags:
Σmll=σ 2
m · Nm−1
∑
n=0 Cnxx ·Vn (6.5.18)
To fit the stochastic model to the observation noise, the amplitude of the covariance
function for each time lag Cnxx must be determined.
If the covariance function were estimated directly in the time domain, the value for one
specific time lag Cnxx could however never change its sign, as the appropriate variance
factor is always estimated as its square (compare eq. (2.6.8)). As the PSD is by definition
always positive, this restriction does not impact its estimation. Negative values of the
covariance function can then occur in the inverse DCT that give the covariance function
from the estimated PSD. Thus, in ITSG-Grace2016, the PSD is estimated instead of the
covariance function, even though the two are functionally interchangeable. This can
be achieved in the spectral domain by determining the amplitude of the PSD at each
frequency Sjxx. Using VCE, the estimated amplitude for each frequency j∈ [0,N) can
be written as
Sˆjxx= αˆ2jS j
xx , (6.5.19)
with Sjxx an a priori value for the amplitude of the PSD at that frequency, and
αˆ2j = Ω˜j
sËœj . (6.5.20)
As the time lag of the covariance function, or conversely the frequency of the PSD,
can appear in any of the covariance matrices Σmll of the M short arcs, depending
Chapter6
ITSG-Grace201664
Contributions to GRACE Gravity Field Recovery
Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Title
- Contributions to GRACE Gravity Field Recovery
- Subtitle
- Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Author
- Matthias Ellmerr
- Publisher
- Verlag der Technischen Universität Graz
- Location
- Graz
- Date
- 2018
- Language
- English
- License
- CC BY 4.0
- ISBN
- 978-3-85125-646-8
- Size
- 21.0 x 29.7 cm
- Pages
- 185
- Keywords
- Geodäsie, Gravitation, Geodesy, Physics, Physik
- Categories
- Naturwissenschaften Physik
- Technik