We used the software package ASCOT (git commit hash daa99c2)Footnote 1 (Artz et al. 2016) for our geodetic analysis. ASCOT is a fully developed geodetic VLBI analysis software package and has been used recently for the contribution of IVS Analysis Center at the Onsala Space Observatory for its contribution to the ITRF2020 calculations.Footnote 2 The software is able to model both thermal (Nothnagel 2009) and gravitational (see, e.g. Nothnagel et al. 2019; Lösler et al. 2019) deformation of radio telescopes, which has a significant impact on the local-tie vectors (see Sect. 5.5.4). ASCOT is also capable of analysing both group-delay and phase-delay observations, and combine the results from multiple databases into one global solution.
A priori data and modelling
ASCOT (and \(\nu \) Solve) make use of a priori data, such as initial station positions, site velocities and Earth Orientation Parameters (EOP). Some of these parameters may have a significant impact on the final results, and therefore we strive to use the best available a priori information.
The ON position was fixed to the value presented in VTRF2020b (BKG 2020). We note that this is the first VTRF release which includes gravitational deformation modelling for ON (Thaller 2021). Initial positions for OE and OW were based on Real-time Kinematic (RTK) GPS measurements carried out in 2016, plus information taken from the construction drawings.
All three stations were assumed to have velocities identical to the values for ONSALA60 in VTRF2020b (BKG 2020). We used axis offsets of 0 mm for OE, OW and \(-6\) mm for ON (Haas and Eschelbach 2005). EOP information was taken from the most recent IERSC04, and the VMF3 tropospheric mapping function (re3data.org 2021) was used in all ASCOT processing.
Source positions of the quasars observed were assumed as their ICRF3 S/X values (Charlot et al. 2020).Footnote 3
Corrections for cable delay variations (CDMS for OTT) were applied in the analysis if, and only if, the antennas had working PCAL which could be used in fringe-fitting. For antennas labelled with Manual PCAL in Table 2, no cable calibration was applied when analysing the particular vgosDb.
No ionosphere corrections
In standard dual- and multi-frequency VLBI observations, ionospheric corrections are usually applied in the analysis. Such corrections were not possible to apply in our case since we only observed X-band. However, the three stations ON, OE and OW are located within about 550 m distance, i.e. the differential ionospheric effects are negligible. Ionospheric corrections could thus be omitted without any significant impact on the analysis.
Pressure correction of observing log files
All three telescope systems at OSO use the same meteorological station, and the corresponding data are recorded identically in the three individual logfiles. However, the ellipsoidal height of this meteosensor is not identical to the ellipsoidal height of neither the reference point (intersection of telescope’s azimuth and elevation axes) of ON, nor of OTT.
We therefore corrected the pressure readings as recorded in log files correspondingly, using a height-dependent pressure correction (Berg 1948). The corrected pressure \(P_n\) is calculated according as
$$\begin{aligned} P_n = P_r \times (1 - 0.0000226\times (h - h_r))^{5.225} \end{aligned}$$
(1)
where \(P_r\) is the original field-system wx log value, h is the height of ON (59.3 m), OE (53.2 m) or OW (53.2 m), and \(h_r\) is the height of the OSO pressure sensor (46.6 m). The approximate changes with respect to the original observing log-values are \(\hbox {ON} = -1.5\) hPa, \(\hbox {OE} = -0.8\) hPa, \(\hbox {OW} = -0.8\) hPa. Since the ellipsoidal heights can be assumed to be accurate within 10 cm, the pressure corrections are expected to be accurate within 0.1 hPa. Using the corrected pressure values in the vgosDbs ensures that the zenith hydrostatic delays can be modelled as good as possible. We note that the log files available via the IVS are the corrected logfiles, with the pressure correction already applied.
Analysis settings and parametrisation
All observed scans were correlated (no data loss), and all correlated scans were post-processed. A few observations were removed in the geodetic analysis, either due to low quality codes from fringe-fitting, or due to being significant outliers. The numbers vary between the vgosDbs, but in general \(>95\%\) of all scheduled observations were used in the final analysis.
In addition to OE and OW station positions, we modelled ZWD (every 30 min), clocks (every 60 min), thermal expansion of the antennas, and gravitational deformation of the antennas. The significance of these effects is investigated in Sect. 5.5.
We also added 3 ps and 1.5 ps of extra elevation-dependent noise to the group- and phase-delay observations, respectively. Addition of extra noise is standard procedure in geodetic VLBI analysis to account for over-optimistic weights in the delay observations, and hence bring the reduced \(\chi ^2\) closer to 1 (Gipson 2007).
Another way to illustrate the results is to look at the OE and OW positions obtained as a function of time, i.e. from each vgosDb. A comparison of the group-delay positions for the 25 ONTIE-session is shown in Fig. 7.
Group-delay analysis
Using ASCOT we obtain, for each vgosDb in Table 2, group-delay position estimates for OE and OW. The OE and OW group-delay positions for all vgosDbs are presented in Tables 11 and 12, respectively. To illustrate the results, we present in Fig. 6 three histograms of the post-fit residuals on the three baselines from the group-delay analysis of all ONTIE-sessions with ASCOT. Normal distributions are fitted to these histograms and show that the mean residuals are below 1 ps on all three baselines, with standard deviations below 15 ps. As expected, the short baseline between the modern VGOS antennas OE and OW gives the best performance.
Station positions derived from global analysis of group-delays
ASCOT allows so-called global solutions, where multiple sessions are combined to estimate one set of coordinates for the whole time span. This is done by stacking the normal equations of the individual sessions into one big normal equation system. By inverting this combined system of normal equations, we obtained the station coordinates of OE and OW, as well as the associated variance-covariance matrix. From the latter, we then calculated the formal uncertainties of the positions. In this combined solution, we only included sessions which had phase and cable calibration applied for all antennas (see Table 2). The resulting global (group-delay) OE and OW positions are given in Table 10.
Phase-delay analysis
With ASCOT we also obtain, for each vgosDb in Table 2, phase-delay position estimates for OE and OW. The OE and OW phase-delay positions for all vgosDbs are presented in Tables 13 and 14, respectively. Histograms of all phase-delay residuals are presented in Fig. 8, with mean residuals below 0.1 ps and standard deviations below 5 ps. This is, as expected, a significant improvement in the uncertainties with respect to the group-delay results. Similarly to our group-delay results, the short baseline between the modern VGOS antennas OE and OW gives the best performance, also for phase-delays.
Table 4 VTRF2020b (epoch 2010.0) phase-delay positions (in m) and their formal standard deviations (in mm) for OE and OW, obtained as described in Sect. 5.3.2
The effect of phase and cable calibration
As noted in Sect. 3.3, ON suffers from direction-dependent cable delay variations (Dan MacMillan, private communication 2002), which will affect the observed delays if not correctly compensated for in the analysis. Indeed, we find a significant systematic offset of about 1 cm in X and Z (see Fig. 9) between experiments with/without PCAL and cable corrections for ON (listed in Table 2).
Station positions from global analysis of phase-delays
As with the group-delay data, we can use ASCOT to obtain a global solution of phase-delay data, i.e. a combined phase-delay solution for multiple sessions. Again, we use the sessions with phase and cable calibration present, and we obtain the OE and OW positions presented in Table 4.
Differences in group-delay and phase-delay positions
Contrary to expectations, we find a significant systematic offset between the group- and phase-delay positions. This can be seen in Fig. 9, where the zero-level is the global group-delay position. However, the offset becomes clearer after conversion to an ENU system, see Table 5. Since the offset is primarily in the Up-direction, it is consistent with an elevation-dependent delay error. ON is known to suffer from significant (\(\sim 5\) mm) gravitational deformation effects, which manifest primarily in the up-coordinate. While this is included in our modelling, this gravitational deformation model was primarily developed and tested using group-delay observations. There could be additional effects which affect phase-delay estimation. Other explanations for this systematic offset are also possible, but a detailed investigation of this offset is beyond the scope of this paper. We note, however, that group-delay analysis is the most common method routinely employed by IVS analysis centres to derive station positions. Therefore, to avoid confusion in the community, we also chose to present group-delay estimates as the OE and OW station positions in this paper. The systematic offset will be monitored and further investigated in future observations.
Table 5 ENU difference for the global OE and OW positions obtained with phase-delays compared to group-delays Modelling clocks, ZWD, and antenna deformation
In this section, we investigate how various effects, which are possible to model in ASCOT, impact the estimated OE and OW positions.
Impact of clock parameter interval length
In order to investigate the impact of the clock parameter interval length, we compared the estimated OTT positions using both 1 h and 20 min intervals. Using 20 min increases the number of parameters to be estimated by a factor of three (compared to 1 h), but did not cause a problem for the analysis due to the large number of observations during the usually 24 h long ONTIE-sessions, with well above 1000 observations per baseline.
Table 6 provides the observed changes in the weighted mean of the estimated station positions for the OTT from all ONTIE-sessions. We find that station positions are not impacted significantly by the choice of clock parameter interval length. This finding is confirmed from a similar analysis of individual ONTIE-sessions with \(\nu \) Solve. Since ON, OE and OW all share the same maser clock, any variations between the three systems are likely due to telescope-specific instrumental instabilities.
Table 6 Effect on the weighted mean station positions of OE and OW when changing from clock interval length of 1 h to 20 min, expressed in a topocentric east-north-up (ENU) coordinate system
Table 7 Effect on the estimated station positions of OE and OW, expressed in a topocentric (ENU) coordinate system, when estimating ZWD for OE and OW as piece-wise linear offsets with 30 min interval length, compared to not estimating ZWD
Impact of estimating Zenith Wet Delay (ZWD)
All three stations are located within 550 m and thus to a large extent share the same common local troposphere. Furthermore, the ONTIE-sessions were scheduled in a way that all three stations observed each scan together, i.e. the antennas had almost identical azimuth and elevation directions. However, in principle, small variations in the local troposphere and atmospheric turbulence effects could affect the delays on the three baselines in a differential way.
Since the elevation angles for the three antennas were almost identical, it is not possible to estimate antenna-specific tropospheric parameters for all three antennas. However, it is possible to estimate differential ZWD parameters for OE and OW as piece-wise linear offsets every 20 min, while not estimating any tropospheric parameters for ON. Table 7 provides the observed changes in the weighted mean of the estimated station positions for the OTT from all ONTIE-sessions when analysing with and without estimating ZWD for OE and OW. The changes are expressed in a topocentric east-north-up (ENU) coordinate system. While the horizontal components are not affected by more than 30 \(\upmu \)m, we note a significant reduction in the up-components of the antennas, on the level of 0.3 mm to 0.8 mm. This shows that estimating differential ZWD is of importance, even for this small network. The estimated differential ZWD themselves are typically within \(\pm 1\) mm, and the values in general follow each other for both stations, with some few exceptions. The overall scatter is on the order of 0.5–1 mm. A more detailed investigation on the differential ZWD and their potential importance to sense atmospheric turbulence, is the topic of future investigations.
Impact of thermal deformation
Figure 10 depicts the expected impact of thermal deformation on a VLBI delay observation for antenna ON and OE/OW following the model by Nothnagel (2009). This delay model uses mainly the antenna dimensions, the expansion coefficients of the material, and the temperature difference with respect to a reference temperature. A temperature of 10 K higher than the reference temperature for the Onsala site is used for this graph. A strong dependence on elevation is visible for both ON and OE/OW. However, since the actual telescope towers have rather similar dimensions, the two curves are rather similar. The largest differential effect for a delay observation on the ON–OE/OW baseline is on the order of 1.5 ps for an observation at zenith direction. Table 8 presents the effect on the estimated weighted mean topocentric positions of OE and OW when including thermal deformation. While the change is largest for the topocentric up-component, none of the changes are significant.
Table 8 Effect of including thermal deformation modelling (Nothnagel 2009) in the analysis
Table 9 Effect of including gravitational deformation modelling (Nothnagel et al. 2019; Lösler et al. 2019) in the data analysis
Table 10 VTRF2020b (epoch 2010.0) group-delay positions (in m) and their formal standard deviations (in mm) for OE and OW, obtained as described in Sect. 5.2.1
Impact of gravitational deformation
Modelling of gravitational deformation of radio telescopes (Nothnagel et al. 2019; Lösler et al. 2019) was not included in ITRF2014, but is strongly recommended by the IVS analysis coordinator, in particular for the preparations for analyses to prepare the upcoming ITRF2020 (John Gipson, private communication, 2020). We therefore used ASCOT to investigate the impact of gravitational deformation on the analysis of the ONTIE-sessions.
Figure 11 depicts the effect of gravitational deformation on the VLBI delay observation for the antennas ON (Nothnagel et al. 2019) and OE/OW (Lösler et al. 2019). Both antenna types again show a clear elevation dependence. However, while OE/OW are rather stiff and stable antennas with a maximum effect of about 2 ps, ON is deforming much more and suffers from delay effects of almost 20 ps between observations in zenith and at the horizon. The largest differential effect for a delay observation on the ON–OE/OW baseline is \(\sim 19\) ps for an observation at the horizon.
Table 9 presents the effects on the estimated weighted mean topocentric positions of OE and OW when these gravitational deformation effects are used or are not used. Using or not using the gravitational deformation model for ON, see Table 9(a), changes the up-component significantly, more than 5.3 mm, while the horizontal changes are not significant. Using or not using the gravitational deformation model for OE and OW, see Table 9(b), also changes the up-component significantly, by more than 0.6 mm, while the horizontal changes are not significant. These tests show the importance of modelling gravitational deformation of VLBI antennas in the data analysis. We note that the consistent modelling of both thermal and gravitational deformation of all three antennas, ON, OE, OW, gives the lowest WRMS scatter of the post-fit residuals.