Web-Books
in the Austria-Forum
Austria-Forum
Web-Books
Naturwissenschaften
Physik
Contributions to GRACE Gravity Field Recovery - Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
Page - 121 -
  • User
  • Version
    • full version
    • text only version
  • Language
    • Deutsch - German
    • English

Page - 121 - 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

Image of the Page - 121 -

Image of the Page - 121 - 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

Text of the Page - 121 -

9.1.1 Total Least Squares as Gauß-Markov Model with Derived Observations Reinking gives a derivation of the solution to the TLS problem in eq. (9.1.4) that relies on the removal of the distinction between dependent and independent variables. Rather, all variables are collected in one vector l= [ ldep lind ] . (9.1.5) Thissectionwillgiveasummaryof thealgorithmpublishedinReinking,2008.Building on this summary, the resulting normal equation system is analysed in preparation for later comparisons with the algorithm presented in section 9.1.2. Reinking’s algorithm begins by restating the problem eq. (9.1.1) in the Gauß-Helmert model as G ( xˆ, lˆ ) = lˆdep−f ( lˆind,xˆ ) =0 . (9.1.6) The functionalG is then linearised about both the parameters and observations, giving G(x0,l0)+ ∂G ∂x ∣∣∣∣ x0,l0 ∆x+ ∂G ∂l ∣∣∣∣ x0,l0 ∆l=0 (9.1.7) or, more compactly, G0+Ax∆x+F∆l=0 . (9.1.8) With∆l= lˆ−l0= l−e−l0, eq. (9.1.8) is G0+Ax∆x+F (l−e−l0)=0 (9.1.9) −Fl−(G0−Fl0)=Ax∆x−Fe (9.1.10) Here, it is important to note that the residuals e are actually residuals in both the dependent and independent variables: e= [ edep eind ] . (9.1.11) Reinking now defines the derived observationsλas λ=−Fl . (9.1.12) With λ0=(G0−Fl0) , (9.1.13) eλ=−Fe , (9.1.14) 9.1 Uncertainties in Independent Variables 121
back to the  book Contributions to GRACE Gravity Field Recovery - Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations"
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
Web-Books
Library
Privacy
Imprint
Austria-Forum
Austria-Forum
Web-Books
Contributions to GRACE Gravity Field Recovery