M.A. Holdaway, Simon J.E. Radford, F.N. Owen, and Scott M. Foster
National Radio Astronomy Observatory
September 26, 1995
r.m.s.
phase
errors at 230 GHz about twice as often as at Mauna Kea. We
also investigate how the residual phase errors depend upon the slew
speed of the antennas
(0.5
s
through 2.0
s
). At 230 GHz, faster
slewing provides a significant improvement in the fraction of time the
array will be able to achieve 30
r.m.s. residual phase errors. At
690 GHz, faster slewing will provide two or three times more observing
time available with 30
r.m.s. residual phase errors. Increasing
the total continuum bandwidth from 4 GHz to 16 GHz provides a marginal
improvement in the residual phase errors.
The primary goal of site testing is to compare site characteristics, such as opacity and phase stability, that will influence astronomical observing. A secondary goal is to predict with some confidence how well various observing strategies, such as fast switching phase calibration, will work. The data analysis for the site test interferometer was outlined in MMA Memo 129 (Holdaway, Radford, Owen, and Foster 1995), and residual phase errors after fast switching were analyzed in MMA Memo 126 (Holdaway and Owen 1995). Here we use the most current estimates of the distributions of the phase structure function and velocity aloft at Chajnantor, Chile, and at the Mauna Kea VLBA site to provide a better picture of how well fast switching will work at these sites.
The analysis of the fast switching phase calibration performed here is identical to the analysis described in MMA Memo 126, but we have changed a number of the input parameters in this work. The differences between the previous work and this work are summarized below:
,
whereas the previous analysis used a velocity of 5ms
\
determined by Colin Masson for the summit of Mauna Kea. We
have used the data reduction path described in MMA Memo 129
(Holdaway, Radford, Owen, and Foster, 1995) to compare the
site test data for the Mauna Kea summit and the Mauna Kea VLBA
site. We found the median velocity aloft for the summit was
about 6ms
, in agreement with Masson's result, but the
median velocity at the lower altitude VLBA
site was 12ms
. This apparent contradiction is understood if the summit
is dominated by surface turbulence that moves across
the interferometer at close to the surface velocity while the
VLBA site is dominated by turbulence at a much higher
elevation. Larger velocities aloft result in larger residual
phase errors with fast switching.
for each simulated calibrator field, resulting in
somewhat larger residual phase errors in most cases.
s
and 2 s setup,
1
s
and 1 s setup, and 2
s
and 0.5 s setup.
Currently the antenna group is confident switching to a
source 1.5
away can be accomplished in about 2 s,
roughly equivalent to 1
s
and 1 s setup.
The residual phase errors after fast switching phase calibration are

(MMA Memo 126), and are independent of baseline length for baselines
longer than
. Note that fast switching phase calibration
will work for arbitrarilly long baselines. The residual phase errors
can be calculated for any simulated calibrator/source configuration,
observing strategy, and instrument sensitivity. Given the
distribution of the structure function,
, we can create a
distribution of residual phase errors that includes both the
distribution of calibrators on the sky and the distribution of
atmospheric conditions. We assume acceptable images can be made with
30
r.m.s. errors.
Figure 1 shows the distributions of residual phase errors after fast switching calibration at Chajnantor with 16 GHz of continuum bandwidth, corrected for 60 degrees elevation angle, calculated for a range of simulated switching speeds. The measured distribution of atmospheric phase fluctuations on a 300 m baseline and the extrapolated distribution of phase fluctuations on a 1000 m baseline are also shown. Figure 2 shows the same distrubutions for Chajnantor with a 4 GHz continuum bandwidth and figures 3 and 4 show the analogous data for the Mauna Kea VLBA site. Figure 5 shows the residual phase error distributions for the Chajnantor and Mauna Kea sites together. Figure 6 shows the residual phase errors improve when a smaller fraction of the cycle time is spent on the target source, making the entire cycle faster since the integration time on the calibrator is fixed.
move from 4 s (0.5
s
and 2 s setup) to 2 s (1
s
and 1 s setup)
would improve the residual phase errors at 230 GHz at Chajnantor
by about
10
, making the array usable about 10% more often.
Observations at 690 GHz would require 10
r.m.s. phase errors on our
230 GHz plots. At 690 GHz, the same improvement would
double the amount of time available for observations.
s
switching, and 16 GHz bandwidth.
If 30
r.m.s.
phase errors are acceptable, spending 83% of the cycle time on the
target source (increasing the noise by 10%) will work just over half
the time. If the atmospheric conditions are marginal, reducing
the source integration to 50% of the cycle time (41%
noise increase) will permit observations with 30
r.m.s.
phase errors 75% of
the time. After this, returns diminish quickly,
since the cycle time, and hence
, will be limited by the slew time,
the distance between source and calibrator, and the detection time
for the calibrator.
Figure 1: Cumulative distributions of residual phase errors at 60 degree elevation
after fast switching with 16 GHz bandwidth at Chajnantor for three
different switching speeds. Distributions of uncorrected atmospheric
phase fluctuations on 300 m and 1000 m baselines are show for
comparison. The two dashed vertical lines represent the 30 degree rms phase
limit required at elevation angle of 60 degrees, and 23 degrees rms phase, which translates
to 30 degrees rms phase at an elevation angle of 30 degrees.
Figure 2: Cumulative distributions of residual phase errors after fast switching
with 4 GHz bandwidth at Chajnantor for three different switching speeds.
Distributions of uncorrected atmospheric phase fluctuations on 300 m
and 1000 m baselines are show for comparison.
Figure 3: Cumulative distributions of residual phase errors after fast switching
with 16 GHz bandwidth at the Mauna Kea VLBA site
for three different switching speeds.
Distributions of uncorrected atmospheric phase fluctuations on 300 m
and 1000 m baselines are show for comparison.
Figure 4: Cumulative distributions of residual phase errors after fast switching
with 4 GHz bandwidth at the Mauna Kea VLBA site
for three different switching speeds.
Distributions of uncorrected atmospheric phase fluctuations on 300 m
and 1000 m baselines are show for comparison.
Figure 5: Comparison of cumulative distributions of residual phase errors
after fast switching with 16 GHz bandwidth at Chajnantor and at Mauna Kea.
Figure 6: Cumulative distributions of residual phase errors
after fast switching at 230 GHz with 16 GHz bandwidth at Chajnantor
for varying fractions of time spent integrating on the target source.
Since the integration time on the calibrator is fixed, smaller fractions
on the target mean faster cycles.
Distributions of uncorrected atmospheric phase fluctuations on 300 m
and 1000 m baselines are show for comparison.
References
Holdaway, M.A., and Ishiguro, Masato, 1995, MMA Memo 127, ``Dependence of Tropospheric Path Length Fluctuations on Airmass.''
Holdaway, M.A., and Owen, F.N., 1995, MMA Memo 126, ``A Test of Fast Switching Phase Calibration with the VLA at 22 GHz.''
Holdaway, M.A., Ishiguro, Masato, and Morita, K.-I., 1995, MMA Memo ???, ``Analysis of the Spatial and Temporal Phase Fluctuations Above Nobeyama.''
Holdaway, M.A., Radford, Simon J.E., Owen, F.N., and Foster, Scott M., 1995, MMA Memo 129, ``Data Processing for Site Test Interferometers.''
Holdaway, M.A., Radford, Simon J.E., Masson, C., Owen, F.N., and Foster, Scott M., 1995, MMA Memo ???, ``Phase Stability Comparison of the VLBA and Millimeter Valley Mauna Kea Sites.''