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AUSAC Meeting March 2-3, 2005 The pointing model 13 term model in az and za with a za lookup table. Latest model created may04 after: –Alfa added (2000+ lbs) –New compressors on dome (450*4 lbs) –Kevlar cables added to stiffen feed tower. –Dome side rollers tightened on 1 side, loosened on the other. Model history (errors in arc seconds). DateAz err asecZa err asecTotal asec
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AUSAC MeetingMarch 2-3 , 2005
Telescope Performance
• Pointing the telescope. • Gain curves for all receivers• Reflector alignment• Recent high frequency results.• Beam widths for all receivers.• Things to work on.
• More info at: http://www.naic.edu/~phil– -> pointing– -> system performance
AUSAC MeetingMarch 2-3 , 2005
Pointing the Telescope• To point the telescope you use:
– Pointing model– Azimuth, za drive systems.– Turret drive system.– 6 Distomats (laser rangers)– Tiedown control system.– Temperature sensor on the platform.– Tertiary drive system (installed but not in use).
• Beam widths of receivers range from:• 900 arc seconds 327 MHz• 28 arc seconds at 10 GHz
• 1/8 inch motion at the horn is 5 arc seconds on the sky.
• Make sure that any errors are repeatable.
AUSAC MeetingMarch 2-3 , 2005
The pointing model• 13 term model in az and za with a za lookup table. • Latest model created may04 after:
– Alfa added (2000+ lbs)– New compressors on dome (450*4 lbs)– Kevlar cables added to stiffen feed tower.– Dome side rollers tightened on 1 side, loosened on the other.
Model history (errors in arc seconds).Date Az err asec Za err asec Total asec1998 3.82 2.37 4.49
1999 5.4 3.1 6.2
2000 5.68 3.45 6.65
2003 5.38 3.48 6.41
2004 4.20 2.41 4.84
AUSAC MeetingMarch 2-3 , 2005
The distomats and tiedowns
• The distomats and tiedowns correct for temperature variation.• 6 distomats (around the rim road) are used to measure the position
of the platform. • Tiedown cables connect each platform corner to a computer
controlled jack in the bowl.
• Operation:– The distomats measure the average platform height every two
minutes.– The computers then drive the tiedowns so the average platform
height remains at a fixed value.• We keep the average height of the platform fixed. We do not keep
the platform level.• Plot shows platform height 05feb05.
AUSAC MeetingMarch 2-3 , 2005
PL Platform hght vs hour
AUSAC MeetingMarch 2-3 , 2005
Distomat failure …
• The distomats fail if it is raining, or if the platform has tilted enough so that the targets are no longer in the distomat beam.
• On failure the computer switches to a temperature sensor on the platform. The differential temperature change from the last good reading is then used to control the tiedowns.
• A 5 deg F change will move the platform 1 inch.
AUSAC MeetingMarch 2-3 , 2005
Tiedown failure
• Large platform tilts and higher temperatures cause a tiedown cable to go slack.
• On 27may04 tension in td 4 was lost during a calibration run:– 10Am, 84degF, za=16.5 az=155.– The td4 jack still had about 8 inches of throw.
• The plot shows the pointing error became > 85 arc seconds.
• The problem is magnified because the computer continues to move the 3 jacks (but only two of them are now moving the platform). This causes the platform to tilt even more.
• Day/evening observing is affected by this. Dome weight is the main culprit.
AUSAC MeetingMarch 2-3 , 2005
Pnt err when td4 looses tension
AUSAC MeetingMarch 2-3 , 2005
Pre 2004 gain Curves
AUSAC MeetingMarch 2-3 , 2005
Curvature of the hi freq gain curves• The curvature in the high frequency gain curves comes from
collimation and focus errors that are a function of az and za.• A 1 lambda focus error is a 3db loss in gain. At 10 Ghz 3cm is 3db
Theodolite surveyJul03 after shimming
AUSAC MeetingMarch 2-3 , 2005
2004 Measurement and Alignment Accomplishments
• Reflector alignment
• Tertiary: Measured and adjusted Oct. 2004– Initial RMS: .9 mm. Final RMS .3 mm.– Measurement Std. Dev. 25 microns
• Secondary: Initially measured Nov. 2003– Final measurments and adjustments May/June 2004– Inital RMS: 1.3 mm. Final RMS: .6 mm.– Measurement Std. Dev. < 50 microns
• Primary: Adjustments Nov. 2004 to Feb. 2005– RMS from last measurement: 1.6 to 1.8 mm.– Measurement Std. Dev. .5 mm– 11,232 points with error larger than 1.5 mm. adjusted– Estimated setting RMS after adjustments: < 1.5 mm.
AUSAC MeetingMarch 2-3 , 2005
Tertiary Setting Errors Prior to AdjustmentsData Taken 21 October 2004
AUSAC MeetingMarch 2-3 , 2005
Tertiary Setting Errors After All Adjustments Data Taken 26 October 2004
AUSAC MeetingMarch 2-3 , 2005
Secondary Setting Errors Prior to AdjustmentsData Taken 11 November 2003
93 points out of 1629 targets missing or off scale
AUSAC MeetingMarch 2-3 , 2005
Secondary Setting Errors After All AdjustmentsData Taken 11 November 2003
11 points out of 1629 targets missing or off scale
AUSAC MeetingMarch 2-3 , 2005
Primary Surface ErrorsPhotos Taken October/November 2001
Histogram of 37889 points, 168 points off scale
RMS of points less than 8mm., 333 points dropped: 1.6mm.RMS of points less than 4 mm., 1393 points dropped: 1.4mm.RMS of points less than 2mm., 7060 points dropped: 1.0mm.RMS of points less than 1.5mm., 11234 points dropped: .8mm.RMS of points less than 1.0mm., 18220 points dropped: .5mm.
AUSAC MeetingMarch 2-3 , 2005
Recent hi freq measurements
• Data taken 01dec04 thru feb05• The plots contain:
– Gain (K/Jy)– Tsys (K)– SEFD (Jy)– Average beamwidth (Asecs)
• A single freq/rcvr is plotted versus za.• Color/symbols are different sources.
AUSAC MeetingMarch 2-3 , 2005
PL Gtsb cb5000
AUSAC MeetingMarch 2-3 , 2005
PL Gtsb cbh7200
AUSAC MeetingMarch 2-3 , 2005
PL Gtsb xb9000
AUSAC MeetingMarch 2-3 , 2005
• System performance vs freq.• Za range limited to 5-14 deg• 4th order poly fit to data• Table contains median values• Scatter from optics.
Rcv GainK/Jy
TsysK
SefdJy
Cb4500 8.6 29.0 3.4Cb4860 8.7 29.9 3.4Cb5000 8.5 30.6 3.6Cb5400 8.1 34.5 4.3Cbh6600 6.0 26.8 4.5
Cbh6900 5.7 25.6 4.6
Cbh7200 5.1 24.1 4.6
Cbh7400 5.0 24.4 4.8
Xb8500 5.0 27.9 5.8Xb8800 5.0 28.4 5.9Xb9000 5.0 29.2 6.1Xb9200 5.0 30.3 6.3
AUSAC MeetingMarch 2-3 , 2005
Beam widths vs. wavelength− HalfPowerBeamWidth = K x lambda/Diameter− HPBW is not sensitive to Cal errors or Flux errors.− HPBW is sensitive to: extended source size, focus and surface errors.− The plots show HPBW measured during 2004 (11600 points).− The illumination lets you trade Tsys for Gain.
Observations:– The dipole feeds have a larger illumination than the horns.
– SBN, CBH horns are under illuminating the dish/tertiary. This gives a smaller Tsys at the expense of the gain.
− The tertiary skirt would let us increase the illumination of the tertiary without a large increase in Tsys. It would also lower Tsys for those receivers that are over illuminating the tertiary.
AUSAC MeetingMarch 2-3 , 2005
AUSAC MeetingMarch 2-3 , 2005
AUSAC MeetingMarch 2-3 , 2005
AUSAC MeetingMarch 2-3 , 2005
AUSAC MeetingMarch 2-3 , 2005
Things to work on1. The dome weight is causing the tiedown/distomats to fail. We need to:
– Make the load cell tension measurements more robust– When low tension in 1 tie down, disable tracking of average height.– Get the tertiary drive system online. Use it to change the focal
length
2. Install the tertiary screen so that receivers that over illuminate the tertiary do not have such a large Tsys (of course this adds weight!!)
3. Measure the pitch/roll/focus errors of the current configuration and then make a new model to try and correct the pitch, roll, focus errors.
4. Continue monitoring the system performance of all receivers for maintenance purposes.