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71.
Younghee Kwak Mathis Bloßfeld Ralf Schmid Detlef Angermann Michael Gerstl Manuela Seitz 《Journal of Geodesy》2018,92(9):1047-1061
The Celestial Reference System (CRS) is currently realized only by Very Long Baseline Interferometry (VLBI) because it is the space geodetic technique that enables observations in that frame. In contrast, the Terrestrial Reference System (TRS) is realized by means of the combination of four space geodetic techniques: Global Navigation Satellite System (GNSS), VLBI, Satellite Laser Ranging (SLR), and Doppler Orbitography and Radiopositioning Integrated by Satellite. The Earth orientation parameters (EOP) are the link between the two types of systems, CRS and TRS. The EOP series of the International Earth Rotation and Reference Systems Service were combined of specifically selected series from various analysis centers. Other EOP series were generated by a simultaneous estimation together with the TRF while the CRF was fixed. Those computation approaches entail inherent inconsistencies between TRF, EOP, and CRF, also because the input data sets are different. A combined normal equation (NEQ) system, which consists of all the parameters, i.e., TRF, EOP, and CRF, would overcome such an inconsistency. In this paper, we simultaneously estimate TRF, EOP, and CRF from an inter-technique combined NEQ using the latest GNSS, VLBI, and SLR data (2005–2015). The results show that the selection of local ties is most critical to the TRF. The combination of pole coordinates is beneficial for the CRF, whereas the combination of \(\varDelta \hbox {UT1}\) results in clear rotations of the estimated CRF. However, the standard deviations of the EOP and the CRF improve by the inter-technique combination which indicates the benefits of a common estimation of all parameters. It became evident that the common determination of TRF, EOP, and CRF systematically influences future ICRF computations at the level of several \(\upmu \)as. Moreover, the CRF is influenced by up to \(50~\upmu \)as if the station coordinates and EOP are dominated by the satellite techniques. 相似文献
72.
Antenna thrust is a small acceleration acting on Global Navigation Satellite System satellites caused by the transmission of radio navigation signals. Knowledge about the transmit power and the mass of the satellites is required for the computation of this effect. The actual transmit power can be obtained from measurements with a high-gain antenna and knowledge about the properties of the transmit and receive antennas as well as losses along the propagation path. Transmit power measurements for different types of GPS, GLONASS, Galileo, and BeiDou-2 satellites were taken with a 30-m dish antenna of the German Aerospace Center (DLR) located at its ground station in Weilheim. For GPS, total L-band transmit power levels of 50–240 W were obtained, 20–135 W for GLONASS, 95–265 W for Galileo, and 130–185 W for BeiDou-2. The transmit power differs usually only slightly for individual spacecraft within one satellite block. An exception are the GLONASS-M satellites where six subgroups with different transmit power levels could be identified. Considering the antenna thrust in precise orbit determination of GNSS satellites decreases the orbital radius by 1–27 mm depending on the transmit power, the satellite mass, and the orbital period. 相似文献
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T. S. R. Babbedge M. Rowan-Robinson M. Vaccari J. A. Surace C. J. Lonsdale D. L. Clements F. Fang D. Farrah A. Franceschini E. Gonzalez-Solares E. Hatziminaoglou C. G. Lacey S. Oliver N. Onyett I. Pérez-Fournon M. Polletta F. Pozzi G. Rodighiero D. L. Shupe B. Siana H. E. Smith 《Monthly notices of the Royal Astronomical Society》2006,370(3):1159-1180
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E. Hatziminaoglou P. Cassata G. Rodighiero I. Pérez-Fournon A. Franceschini A. Hernán-Caballero F. M. Montenegro-Montes A. Afonso-Luis T. Jarrett G. Stacey C. Lonsdale F. Fang S. Oliver M. Rowan-Robinson D. Shupe H. E. Smith J. Surace C. K. Xu E. A. González-Solares 《Monthly notices of the Royal Astronomical Society》2005,364(1):47-58
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