Seite - 95 - 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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0.1 1 10 100
Frequency [mHz]
10−11
10−9
10−7
10−5
KBR
LRI
Figure 7.7: Real data. Propagation of orbit noise to range rate measurement ρ˙. Solid
black is a noise model for the GRACE KBR and ACC instrument noise,
Dashed black is a noise model for the GRACE-FO LRI and ACC
instruments. The other colours are the same as in figs. 7.4 to 7.6.
range-rate error smaller than the precision of the current KBR instrument on GRACE
(solid black line) across the entire frequency spectrum.
Inthebranchoftheerrorspectrumthat isdominatedbytheKBRnoise,above≈10mHz,
the accuracy of the configuration using no reference motion (brown) as well as the
uncertainty of both the Kepler configurations (pink and green) are well above the
performance estimate for the LRI (dashed black line). Both configurations using
equinoctial elements (purple and orange) are below the LRI noise level over the
complete spectrum. As could be expected, the equinoctial configuration based on the
best-fit reference ellipse (orange) also shows the lowest noise in this domain.
The KBR noise spectrum in fig. 7.7 is based on spectral analysis of real GRACE SST
residuals. The performance estimate for the LRI is based on real GRACE ACC data,
a description of the noise characteristics of the LRI (Heinzel et al., 2012), and an
optimistic assumption of a 50-fold improvement of the ranging accuracy with regard
to the KBR instrument (Flechtner, 2012).
7.4 Discussion
An improved algorithm for dynamic orbit determination was developed, paying
particular attention to its applicability to GRACE-FO data processing. The existing
methodology was refined by applying Encke’s method, directly eliminating the large
contribution of the central term of Earth’s gravitational potential on the numerically
integrated accelerations. Encke’s method was then refined in two separate ways: First,
the osculating reference ellipse proposed by Encke was replaced by a rigorously
optimized best-fit reference ellipse. Such a best-fit ellipse significantly reduces the
7.4 Discussion 95
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