Details
Original language | English |
---|---|
Journal | Hannover : Institutionelles Repositorium der Leibniz Universität Hannover |
Publication status | Published - 13 Apr 2018 |
Abstract
Cite this
- Standard
- Harvard
- Apa
- Vancouver
- BibTeX
- RIS
In: Hannover : Institutionelles Repositorium der Leibniz Universität Hannover, 13.04.2018.
Research output: Contribution to journal › Article › Research
}
TY - JOUR
T1 - IfE monthly gravity field solutions using the variational equations
AU - Naeimi, Majid
AU - Koch, Igor
AU - Khami, Arman
AU - Flury, Jakob
PY - 2018/4/13
Y1 - 2018/4/13
N2 - In this contribution, we present the LUH-GRACE2018 monthly gravity field solutions from GRACE-KBR measurements, which produced at Institut für Erdmessung (IfE) at Leibniz University of Hannover. Our solutions, based on the classical variational approach, are obtained in two processing steps. In the first step, the orbits of both satellites are dynamically integrated and the initial state vectors together with accelerometer bias parameters of both satellites are adjusted using GRACE L1B reduced dynamic orbit. In the second step the 6-hourly-arc normal equations are accumulated and the monthly gravity field spherical coefficients up to degree and order 80 are estimated along with the unknown parameters of step 1. The geoid degree standard deviations of our solutions show a very good agreement with the official solutions of CSR, GFZ and JPL. The differences are well below 0.1 of an order of magnitude indicating the success of our implementation. Details of processing steps and the mass variations derived from our solutions are presented.
AB - In this contribution, we present the LUH-GRACE2018 monthly gravity field solutions from GRACE-KBR measurements, which produced at Institut für Erdmessung (IfE) at Leibniz University of Hannover. Our solutions, based on the classical variational approach, are obtained in two processing steps. In the first step, the orbits of both satellites are dynamically integrated and the initial state vectors together with accelerometer bias parameters of both satellites are adjusted using GRACE L1B reduced dynamic orbit. In the second step the 6-hourly-arc normal equations are accumulated and the monthly gravity field spherical coefficients up to degree and order 80 are estimated along with the unknown parameters of step 1. The geoid degree standard deviations of our solutions show a very good agreement with the official solutions of CSR, GFZ and JPL. The differences are well below 0.1 of an order of magnitude indicating the success of our implementation. Details of processing steps and the mass variations derived from our solutions are presented.
UR - https://www.repo.uni-hannover.de/handle/123456789/4492
U2 - 10.15488/4452
DO - 10.15488/4452
M3 - Article
JO - Hannover : Institutionelles Repositorium der Leibniz Universität Hannover
JF - Hannover : Institutionelles Repositorium der Leibniz Universität Hannover
ER -