Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Leos Mervart"'
Publikováno v:
ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation.
Publikováno v:
ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation.
Publikováno v:
Beutler, Gerhard; Jäggi, Adrian; Hugentobler, Urs; Mervart, Leos (2006). Efficient satellite orbit modelling using pseudo-stochastic parameters. Journal of geodesy, 80(7), pp. 353-372. Berlin: Springer-Verlag 10.1007/s00190-006-0072-6
If the force field acting on an artificial Earth satellite is not known a priori with sufficient accuracy to represent its observations on their accuracy level, one may introduce so-called pseudo-stochastic parameters into an orbit determination proc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb08c8a123286a7cd2bfedafda1912cd
http://doc.rero.ch/record/321361/files/190_2006_Article_72.pdf
http://doc.rero.ch/record/321361/files/190_2006_Article_72.pdf
Publikováno v:
Bertone, Stefano; Arnold, Daniel; Jäggi, Adrian; Beutler, Gerhard; Mervart, Leo (2014). GRAIL Gravity Field Determination Using the Celestial Mechanics Approach. In: AGU Fall Meeting 2014. San Francisco, California, USA. 15.12.-19.12.2014.
Icarus
Icarus
The NASA mission GRAIL (Gravity Recovery and Interior Laboratory) inherited its concept from the GRACE (Gravity Recovery and Climate Experiment) mission to determine the gravity field of the Moon. We present lunar gravity fields based on the data of
Autor:
Krzysztof Sośnica, Lars Prange, Daniel Arnold, Rolf Dach, Simon Lutz, Stefan Schaer, Michael Meindl, Leos Mervart, Adrian Jäggi, Gerhard Beutler
Publikováno v:
Arnold, Daniel; Meindl, Michael; Beutler, Gerhard; Dach, Rolf; Schaer, Stefan; Lutz, Simon; Prange, Lars; Sosnica, Krzysztof Jakub; Mervart, Leos; Jäggi, Adrian (2015). CODE’s new solar radiation pressure model for GNSS orbit determination. Journal of geodesy, 89(8), pp. 775-791. Springer 10.1007/s00190-015-0814-4
The Empirical CODE Orbit Model (ECOM) of the Center for Orbit Determination in Europe (CODE), which was developed in the early 1990s, is widely used in the International GNSS Service (IGS) community. For a rather long time, spurious spectral lines ar
Publikováno v:
Advances in Space Research. 45:215-224
The gravity field model AIUB-CHAMP02S, which is based on six years of CHAMP GPS data, is presented here. The gravity field parameters were derived using a two step procedure: In a first step a kinematic trajectory of a low Earth orbiting (LEO) satell
Publikováno v:
VIII Hotine-Marussi Symposium on Mathematical Geodesy ISBN: 9783319245485
The Gravity Recovery And Interior Laboratory (GRAIL) mission orbiting the Moon and the Gravity Recovery And Climate Experiment (GRACE) mission orbiting the Earth share many conceptual commonalities. Major differences reside, however, in the absolute
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5ce710e32c6a038ba29b6e80aa066434
Autor:
Jan Dousa, Leos Mervart
Publikováno v:
Physics and Chemistry of the Earth, Part A: Solid Earth and Geodesy. 26:555-560
We present here our hourly orbit product and we compare it to other near real-time (NRT) reliable orbits. The comparisons are based on satellite position differences with respect to the final IGS orbits. Experience shows that the use of predicted pre
Publikováno v:
Journal of Geodesy. 70:287-299
The final products of theCODE Analysis Center (Center for Orbit Determination in Europe) of theInternational GPS Service for Geodynamics (IGS) stem fromoverlapping 3-day-arcs. Until 31 December, 1994 these long arcs were computedfrom scratch, i.e. by
Ambiguity resolution strategies using the results of the International GPS Geodynamics Service (IGS)
Publikováno v:
Bulletin Géodésique. 68:29-38
Resolving the initial phase ambiguities of GPS carrier phase observations was always considered an important aspect of GPS processing techniques. Resolution of the so-called wide-lane ambiguities using a special linear combination of theL1 andL2 carr