Page - 63 - 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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6.5.2 Covariance Function and Power Spectral Density
For a wide-sense stationary process such as the assumed observation noise, the co-
variance function of the process and the power spectral density (PSD) of the process
form a Fourier pair (Etten, 2006). As the covariance function describing the observation
noise is only estimated and known in its discretised form, a discrete transform to the
spectral domain is used to compute the PSD. For ITSG-Grace2016, the type I discrete
cosine transform (DCT) is used (Rao and Yip, 1990). This transform implies that the
covariance function is even at the origin, with
C−nxx =Cnxx (6.5.9)
and also even at the upper boundary of the domain, with
CNmax−nxx =CNmax+nxx . (6.5.10)
As the DCT is a linear operator, it can be written as
x˜=Xx , (6.5.11)
withX the N×N matrix of DCT coefficients,xan N×1 vector of equidistant data
points in the time domain, and x˜ the N×1 DCT of x. The elements of the DCT
matrixX are (see e.g. Rao and Yip, 1990, p. 11)
Xmn= √
2
N−1 (
kmkncos (
mnpi
N−1 ))
, m,n∈ [0,N) , (6.5.12)
with
ki= {
1 if i 6=0
1√
2 otherwise. (6.5.13)
The PSD of the observation noise is then, in terms of the covariance function,
Sxx=XCxx . (6.5.14)
The elements of the PSD are
Sjxx=Sxx(fj) , j∈ [0,N) . (6.5.15)
with f0 = 0Hz and fN−1 the Nyquist frequency of the signal. Each entry gives the
amplitude of the observation noise at that specific frequency.
6.5.3 Estimation of Covariance Function
The Toeplitz cofactor matrix for each observation type can be written as a sum of Nmax
individual cofactor matrices, each only dependent on the covariance function of one
6.5 Fit of Stochastic Model 63
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