Anno Löcher
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Anno Löcher has a total of 11 co-authors. Here are the top co-authors by number of shared publications:
- Jürgen Kusche
Institute of Geodesy and Geoinformation University of Bonn Bonn Germany
4 shared publications - Christina Lück
Institute of Geodesy and Geoinformation, University of Bonn, Nußallee 17, 53115 Bonn, Germany
1 shared publication - Ehsan Forootan
Geodesy Group, Department of Sustainability and Planning, Aalborg University, Rendsburggade 14, Aalborg, 9000, Denmark
1 shared publication - Franz Hofmann
Leibniz Universität Hannover
1 shared publication - Isabel Haase
Technical University Berlin (TUB), Dept. of Planetary Geodesy, 10623 Berlin, Germany
1 shared publication Jürgen Kusche
Institut für Geodäsie und Geoinformation, Universität Bonn, Bonn, Germany
1 shared publication
Latest Publications
- Open Access
- 23 December 2020
- Published by Springer Nature in Journal of Geodesy
- Vol. 95 (1) , 1-15
A hybrid approach for recovering high-resolution temporal gravity fields from satellite laser ranging
A new approach to recover time-variable gravity fields from satellite laser ranging (SLR) is presented. It takes up the concept of lumped coefficients by representing the temporal changes of the Earth’s gravity field by spatial patterns via combinations of spherical harmonics. These patterns are derived from the GRACE mission by decomposing the series of monthly gravity field solutions into empirical orthogonal functions (EOFs). The basic idea of the approach is then to use the leading EOFs as base functions in the gravity field modelling and to adjust the respective scaling factors straightforward within the dynamic orbit computation; only for the lowest degrees, the spherical harmonic coefficients are estimated separately. As a result, the estimated gravity fields have formally the same spatial resolution as GRACE. It is shown that, within the GRACE time frame, both the secular and the seasonal signals in the GRACE time series are reproduced with high accuracy. In the period prior to GRACE, the SLR solutions are in good agreement with other techniques and models and confirm, for instance, that the Greenland ice sheet was stable until the late 1990s. Further validation is done with the first monthly fields from GRACE Follow-On, showing a similar agreement as with GRACE itself. Significant differences to the reference data only emerge occasionally when zooming into smaller river basins with strong interannual mass variations. In such cases, the approach reaches its limits which are set by the low spectral sensitivity of the SLR satellites and the strong constraints exerted by the EOFs. The benefit achieved by the enhanced spatial resolution has to be seen, therefore, primarily in the proper capturing of the mass signal in medium or large areas rather than in the opportunity to focus on isolated spatial details.
- 23 December 2020
- Published by Springer Nature in Journal of Geodesy
- Vol. 95 (1) , 1-15
Open AccessA hybrid approach for recovering high-resolution temporal gravity fields from satellite laser ranging
A new approach to recover time-variable gravity fields from satellite laser ranging (SLR) is presented. It takes up the concept of lumped coefficients by representing the temporal changes of the Earth’s gravity field by spatial patterns via combinations of spherical harmonics. These patterns are derived from the GRACE mission by decomposing the series of monthly gravity field solutions into empirical orthogonal functions (EOFs). The basic idea of the approach is then to use the leading EOFs as base functions in the gravity field modelling and to adjust the respective scaling factors straightforward within the dynamic orbit computation; only for the lowest degrees, the spherical harmonic coefficients are estimated separately. As a result, the estimated gravity fields have formally the same spatial resolution as GRACE. It is shown that, within the GRACE time frame, both the secular and the seasonal signals in the GRACE time series are reproduced with high accuracy. In the period prior to GRACE, the SLR solutions are in good agreement with other techniques and models and confirm, for instance, that the Greenland ice sheet was stable until the late 1990s. Further validation is done with the first monthly fields from GRACE Follow-On, showing a similar agreement as with GRACE itself. Significant differences to the reference data only emerge occasionally when zooming into smaller river basins with strong interannual mass variations. In such cases, the approach reaches its limits which are set by the low spectral sensitivity of the SLR satellites and the strong constraints exerted by the EOFs. The benefit achieved by the enhanced spatial resolution has to be seen, therefore, primarily in the proper capturing of the mass signal in medium or large areas rather than in the opportunity to focus on isolated spatial details.
- 21 September 2018
- Published by Springer Nature in Journal of Geodesy
- Vol. 93 (11) , 2421-2428
Assessment of the impact of one-way laser ranging on orbit determination of the Lunar Reconnaissance Orbiter
- 21 September 2018
- Published by Springer Nature in Journal of Geodesy
- Vol. 93 (11) , 2421-2428
Assessment of the impact of one-way laser ranging on orbit determination of the Lunar Reconnaissance Orbiter
- Open Access
- 18 May 2018
- Published by Copernicus GmbH in Annales Geophysicae
- Vol. 36 (3) , 761-779
Comparison of accelerometer data calibration methods used in thermospheric neutral density estimation
Ultra-sensitive space-borne accelerometers on board of low Earth orbit (LEO) satellites are used to measure non-gravitational forces acting on the surface of these satellites. These forces consist of the Earth radiation pressure, the solar radiation pressure and the atmospheric drag, where the first two are caused by the radiation emitted from the Earth and the Sun, respectively, and the latter is related to the thermospheric density. On-board accelerometer measurements contain systematic errors, which need to be mitigated by applying a calibration before their use in gravity recovery or thermospheric neutral density estimations. Therefore, we improve, apply and compare three calibration procedures: (1) a multi-step numerical estimation approach, which is based on the numerical differentiation of the kinematic orbits of LEO satellites; (2) a calibration of accelerometer observations within the dynamic precise orbit determination procedure and (3) a comparison of observed to modeled forces acting on the surface of LEO satellites. Here, accelerometer measurements obtained by the Gravity Recovery And Climate Experiment (GRACE) are used. Time series of bias and scale factor derived from the three calibration procedures are found to be different in timescales of a few days to months. Results are more similar (statistically significant) when considering longer timescales, from which the results of approach (1) and (2) show better agreement to those of approach (3) during medium and high solar activity. Calibrated accelerometer observations are then applied to estimate thermospheric neutral densities. Differences between accelerometer-based density estimations and those from empirical neutral density models, e.g., NRLMSISE-00, are observed to be significant during quiet periods, on average 22 % of the simulated densities (during low solar activity), and up to 28 % during high solar activity. Therefore, daily corrections are estimated for neutral densities derived from NRLMSISE-00. Our results indicate that these corrections improve model-based density simulations in order to provide density estimates at locations outside the vicinity of the GRACE satellites, in particular during the period of high solar/magnetic activity, e.g., during the St. Patrick's Day storm on 17 March 2015.
- 18 May 2018
- Published by Copernicus GmbH in Annales Geophysicae
- Vol. 36 (3) , 761-779
Open AccessComparison of accelerometer data calibration methods used in thermospheric neutral density estimation
Ultra-sensitive space-borne accelerometers on board of low Earth orbit (LEO) satellites are used to measure non-gravitational forces acting on the surface of these satellites. These forces consist of the Earth radiation pressure, the solar radiation pressure and the atmospheric drag, where the first two are caused by the radiation emitted from the Earth and the Sun, respectively, and the latter is related to the thermospheric density. On-board accelerometer measurements contain systematic errors, which need to be mitigated by applying a calibration before their use in gravity recovery or thermospheric neutral density estimations. Therefore, we improve, apply and compare three calibration procedures: (1) a multi-step numerical estimation approach, which is based on the numerical differentiation of the kinematic orbits of LEO satellites; (2) a calibration of accelerometer observations within the dynamic precise orbit determination procedure and (3) a comparison of observed to modeled forces acting on the surface of LEO satellites. Here, accelerometer measurements obtained by the Gravity Recovery And Climate Experiment (GRACE) are used. Time series of bias and scale factor derived from the three calibration procedures are found to be different in timescales of a few days to months. Results are more similar (statistically significant) when considering longer timescales, from which the results of approach (1) and (2) show better agreement to those of approach (3) during medium and high solar activity. Calibrated accelerometer observations are then applied to estimate thermospheric neutral densities. Differences between accelerometer-based density estimations and those from empirical neutral density models, e.g., NRLMSISE-00, are observed to be significant during quiet periods, on average 22 % of the simulated densities (during low solar activity), and up to 28 % during high solar activity. Therefore, daily corrections are estimated for neutral densities derived from NRLMSISE-00. Our results indicate that these corrections improve model-based density simulations in order to provide density estimates at locations outside the vicinity of the GRACE satellites, in particular during the period of high solar/magnetic activity, e.g., during the St. Patrick's Day storm on 17 March 2015.
- 26 February 2018
- Published by Springer Nature in Journal of Geodesy
- Vol. 92 (9) , 989-1001
Precise orbits of the Lunar Reconnaissance Orbiter from radiometric tracking data
- 26 February 2018
- Published by Springer Nature in Journal of Geodesy
- Vol. 92 (9) , 989-1001
Precise orbits of the Lunar Reconnaissance Orbiter from radiometric tracking data
- 1 January 2015
- Published by Springer Nature
- p. 201-207
Towards Improved Lunar Reference Frames: LRO Orbit Determination
- 1 January 2015
- Published by Springer Nature
- p. 201-207
Towards Improved Lunar Reference Frames: LRO Orbit Determination