Gabriele Giorgi

Dr. Gabriele Giorgi


Research Focus & Metrics

Academic Career Length

18Years (2009-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

View All Publications
4 December 2018 in Physical Review Letters
Verified
Journal Article
Closed access
PDF file
SHSven Herrmann
Sven Herrmann
FFFelix Finke
Felix Finke
MLMartin Lülf
Martin Lülf
OKOlga Kichakova
Olga Kichakova
DPDirk Puetzfeld
Dirk Puetzfeld
CLClaus Lämmerzahl
Claus Lämmerzahl
On August 22, 2014, the satellites GSAT-0201 and GSAT-0202 of the European GNSS Galileo were unintentionally launched into eccentric orbits. Unexpectedly, this has become a fortunate scientific opportunity since the onboard hydrogen masers allow for a sensitive test of the redshift predicted by the theory of general relativity. In the present Letter, we describe an analysis of approximately three years of data from these satellites including three different clocks. For one of these, we determine the test parameter quantifying a potential violation of the combined effects of the gravitational redshift and the relativistic Doppler shift. The uncertainty of our result is reduced by more than a factor 4 as compared to the values of Gravity Probe A obtained in 1976.

13 March 2010 in GPS Solutions
Verified
Journal Article
Open access
PDF file
Peter TeunissenPeter Teunissen
Peter Teunissen
GGGabriele Giorgi
Gabriele Giorgi
PBP. J. Buist
P. J. Buist
Global navigation satellite system (GNSS) ambiguity resolution is the process of resolving the unknown cycle ambiguities of the carrier phase data as integers. The sole purpose of ambiguity resolution is to use the integer ambiguity constraints as a means of improving significantly on the precision of the remaining GNSS model parameters. In this contribution, we consider the problem of ambiguity resolution for GNSS attitude determination. We analyse the performance of a new ambiguity resolution method for GNSS attitude determination. As it will be shown, this method provides a numerically efficient, highly reliable and robust solution of the nonlinearly constrained integer least-squares GNSS compass estimators. The analyses have been done by means of a unique set of extensive experimental tests, using simulated as well as actual GNSS data and using receivers of different manufacturers and type as well as different platforms. The executed field tests cover two static land experiments, one in the Netherlands and one in Australia, and two dynamic experiments, a low-dynamics vessel experiment and high-dynamics aircraft experiment. In our analyses, we focus on stand-alone, unaided, single-frequency, single-epoch attitude determination, as this is the most challenging case of GNSS compass processing.

1 September 2019 in Advances In Space Research
Verified
Journal Article
Closed access
GGGabriele Giorgi
Gabriele Giorgi
TST.D. Schmidt
T.D. Schmidt
CTC. Trainotti
C. Trainotti
RMR. Mata-Calvo
R. Mata-Calvo
CFC. Fuchs
C. Fuchs
HSH. Schuh
H. Schuh

1 July 2010 in Advances In Space Research
Verified
Journal Article
Closed access
GGGabriele Giorgi
Gabriele Giorgi
Peter TeunissenPeter Teunissen
Peter Teunissen
SVSandra Verhagen
Sandra Verhagen
PBPeter J. Buist
Peter J. Buist

1 October 2017 in Acta Astronautica
Verified
Journal Article
Closed access
HMHarvey Gómez Martínez
Harvey Gómez Martínez
GGGabriele Giorgi
Gabriele Giorgi
BEBernd Eissfeller
Bernd Eissfeller

1 January 2012 in Journal of Guidance, Control, and Dynamics
Verified
Journal Article
Closed access
GGGabriele Giorgi
Gabriele Giorgi
Peter TeunissenPeter Teunissen
Peter Teunissen
SVSandra Verhagen
Sandra Verhagen
PBPeter J. Buist
Peter J. Buist