Page - 108 - 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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0.00.20.40.6
PDFof σˆAOC,A 0
1
2
3
4
5
6
GRACE-A
0.0 0.2 0.4 0.6
PDFof σˆAOC,B
GRACE-B
Figure 8.5: Kernel density estimate of PDFs of estimated AOC variance
factors σˆAOC,A/B for complete GRACE time series. Each barb represents
one variance factor for one month.
8.3.2 Arc-wise Variance Factors
The AOC covariance matrices, scaled by their variance factors, are expected to model
some of the increased noise in observations with large opening angles. It is thus
expected that the increase in the arc-wise variance factors for the stationary noise com-
ponent previously observed for these time periods should, to some extent, disappear.
One such period is the time that GRACE-A spent in attitude hold mode in June 2010,
mentioned before in section 6.5 and seen in the arc-wise variance factors displayed in
fig. 6.8b.
Figure 8.6a illustrates the arc-wise variance factors for the same data in June 2010,
using the improved stochastic model. The arc-wise variance factors for the stochastic
model considering only the estimated stationary covariance function (in brown) again
shows the increase in arc-wise variance factors during the period of increased opening
angles (darker shaded area). Introducing the a priori AOC covariance information for
this month (in blue), the estimated arc-wise variance factors are noticeably closer to
1 during this period. The same effect can be observed in other periods of increased
opening angles, for example the orbit swap manoeuvre in December 2005 when both
GRACE-A and GRACE-B were commanded to attitude hold mode. In addition the
1° pitch bias that keeps the KBR horns in alignment was removed, leading to very
large angles during the periods when a KBR link was established. Figure 8.6b shows
that during this period the arc-wise variance factors for the processing using the AOC
covariance information (in blue) are again much improved.
Chapter8 Star Camera Observations and
Uncertainties108
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