Seite - 135 - 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
Bild der Seite - 135 -
Text der Seite - 135 -
9.3.3 Effect on Antenna Offset Correction
After each iteration of the TLS adjustment the estimated orientations are used to
re-compute the antenna offset correction. This leads to a new improved antenna offset
correction that is slightly different from the initial AOC computed from the SCA/ACC
sensor fusion orientation. As the AOC is a non-stationary process, analysing its change
in the spectral domain would be fallacious. Instead, the change of magnitude of the
AOC at each epoch is analysed, which is not dependent on the absolute value of the
AOC. For a month of regular data, e.g. April 2008, the mean magnitude of the AOC
is≈3.8 ·10−8m/s. The mean of the estimated correction due to the improved TLS
orientation estimate for the same month is≈3.5 ·10−9m/s, which is roughly one order
of magnitude smaller. For other months, the magnitude of both the AOC and the
correction can be significantly larger.
Figure 9.5 shows the distribution of these deviations
dAOC(τ)= AOCnew(τ)
AOCold(τ) −1 (9.3.1)
in percent. A value below 0% indicates that the new AOC for that epoch is smaller
than the original, a value larger than 0% represents an increased AOC. As these
deviations are computed in the range-rate domain, a translation of this change into a
statement on the magnitude of the opening angle β is not directly possible. Instead,
a smaller value for dAOC indicates a slower change in the opening angle, with a
larger value representing a faster change. All curves are skewed very slightly towards
negative values, indicating that the TLS estimate of the orientation tends to dampen
high-velocity motion in the satellite pointing.
−100 −75 −50 −25 0 25 50 75 100
Deviation in AOC dAOC due to ∆αˆ [%]
0.00
0.01
0.02
0.03 Two SCA heads active:
Both spacecraft
Neither spacecraft
GRACE-A only
GRACE-B only
Figure 9.5: Distribution of change in AOC due to improved orientation in relation to
the magnitude of the original AOC. The data sets underlying the separate
distributions were selected according to how many SCA heads were active
for the respective epochs.
9.3 Results 135
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