Per workpermit 5758 installed the new Beckhoff based vacuum control chassis and computer. There were a couple of hardware issues. First was the polarity of the 4-20ma inputs. One set of 4 for the fan vibration monitors were fine but we had to swap the 3 for vacuum LN2 gauges. Also plugged the Watchdog shorting connector in backwards which prevented the LN2 control valve from operating. Once we fixed those issues the hardware and Beckhoff software worked fine. The next problem was the gateway computer. Some files needed to be modified to allow the channels to pass. I will let other comment on this. For now the system is running and screens are being modified so the users will not see much difference.
I wrote a quick script that will change all of the gains in the appropriate degrees of freedom for the SEI Corner Station sensor correction. The gains should be 0 or OFF when recentering the STS, and then turned back ON after (assuming the chambers are up). I imagine there will be more guidence for operators to do this in the future.
The script can be found in (userapps)/isi/h1/scripts/Toggle_CS_Sensor_Correction.py
thomas.shaffer@opsws10:/opt/rtcds/userapps/release/isi/h1/scripts$ ./Toggle_CS_Sensor_Correction.py -h
usage: Toggle_CS_Sensor_Correction.py [-h] ON_or_OFF
positional arguments:
ON_or_OFF 1 or 0 to turn the gain ON or OFF respectively
optional arguments:
-h, --help show this help message and exit
WP 5765 See T1600062 SEI log 897
Changed data storage rate for BSC:
1) ISI-optic_STi_MASTER_H(V)j_DRIVE & ST2_BLND_dof_GS13_CUR_IN1
This change means that for the next week or so, inquiries of these channels for times from ~5 days ago to before the restart will need to be via nds2. And, one must avoid selecting a request or data that spans the change. Middle of a maintenance day...maybe that should just be avoided anyway.
2) Increased allowable saturations on L4Cs, GS13s & ACTs to reduce unwarranted tripping.
3) Replaced some utility channels with lower case characters with upper case.
4) Replaced a momentary with LONG_PULSE for STS2 mass centering function.
5) Added SUS Point calculation blocks (detailed in 25913.) ISI will take the overhead of calculating this to ease the load of the SUS model.
6) Added Stage2 senscorr DQ channels for T240 & CPS.
The LVEA main crane rail shimming as suggested by the survey crew from Duane Hartman & Associates Inc. has been completed. A copy of the shim changes will be entered in the DCC soon.
The attached plot (and script) shows the nominal TCS power levels required for O2 to correct for just the ITM substrate lenses.
The following values are assumed:
The bottom line is that we will cease to need central heating around 45W on ITMX and 30W on ITMY and will need to start using the RHs to compensate for the thermal lenses. No consideration is yet given to HOM correction with annular CO2 heating.
Subject: Re: RC as-built designDate: May 14, 2015 at 7:54:37 PM EDT
Hi All,
The value of the thermal lens that was always used when adjusting the cavities is 50 km.
The issue which caused all of the confusion last summer was one of definition; i.e. what does it mean to have a 50 km thermal lens. The plots Muzammil put together, on which the decision to include the thermal lens was based, modeled the thermal lens as being inside the ITM. The model we used to adjust the optic positions had the 50 km thermal lens immediately in front of the ITM. The effective focal length in the two cases differs by a factor of n (the index of refraction), with it being stronger in the model which was used to calculate the positions. Because of this the positions were tuned to have a slightly stronger thermal lens than was originally decided on based on Muzammil's plots.
Fortunately, Lisa and I discovered that this is essentially a non-issue since the length changes needed to tune for the two different thermal lenses are less than the length changes needed to compensate for tolerances in the measured radii of curvature of the optics.
Thank you Aidan for working on this.
Speaking of the thermal lensing, we (the LHO crews) have been discussing a possible TCS pre-loading strategy. Here are some summary points of our (future) strategy:
Any comments/questions are welcome.
All T240s prrof masses that within healthy range (< 0.3 [V]). Great!
Here's a list of how they're doing just in case you care:
ETMX T240 1 DOF X/U = 0.077 [V]
ETMX T240 1 DOF Y/V = 0.094 [V]
ETMX T240 1 DOF Z/W = 0.119 [V]
ETMX T240 2 DOF X/U = -0.199 [V]
ETMX T240 2 DOF Y/V = -0.246 [V]
ETMX T240 2 DOF Z/W = -0.094 [V]
ETMX T240 3 DOF X/U = 0.093 [V]
ETMX T240 3 DOF Y/V = -0.087 [V]
ETMX T240 3 DOF Z/W = 0.06 [V]
ETMY T240 1 DOF X/U = 0.03 [V]
ETMY T240 1 DOF Y/V = -0.042 [V]
ETMY T240 1 DOF Z/W = 0.005 [V]
ETMY T240 2 DOF X/U = -0.168 [V]
ETMY T240 2 DOF Y/V = 0.029 [V]
ETMY T240 2 DOF Z/W = 0.132 [V]
ETMY T240 3 DOF X/U = -0.001 [V]
ETMY T240 3 DOF Y/V = -0.003 [V]
ETMY T240 3 DOF Z/W = 0.1 [V]
ITMX T240 1 DOF X/U = -0.023 [V]
ITMX T240 1 DOF Y/V = 0.275 [V]
ITMX T240 1 DOF Z/W = 0.202 [V]
ITMX T240 2 DOF X/U = 0.24 [V]
ITMX T240 2 DOF Y/V = 0.262 [V]
ITMX T240 2 DOF Z/W = 0.296 [V]
ITMX T240 3 DOF X/U = 0.064 [V]
ITMX T240 3 DOF Y/V = 0.247 [V]
ITMX T240 3 DOF Z/W = 0.239 [V]
ITMY T240 1 DOF X/U = 0.192 [V]
ITMY T240 1 DOF Y/V = 0.068 [V]
ITMY T240 1 DOF Z/W = 0.116 [V]
ITMY T240 2 DOF X/U = 0.196 [V]
ITMY T240 2 DOF Y/V = 0.266 [V]
ITMY T240 2 DOF Z/W = 0.214 [V]
ITMY T240 3 DOF X/U = 0.121 [V]
ITMY T240 3 DOF Y/V = 0.214 [V]
ITMY T240 3 DOF Z/W = -0.149 [V]
BS T240 1 DOF X/U = 0.054 [V]
BS T240 1 DOF Y/V = 0.091 [V]
BS T240 1 DOF Z/W = 0.22 [V]
BS T240 2 DOF X/U = 0.162 [V]
BS T240 2 DOF Y/V = 0.237 [V]
BS T240 2 DOF Z/W = 0.231 [V]
BS T240 3 DOF X/U = 0.134 [V]
BS T240 3 DOF Y/V = 0.087 [V]
BS T240 3 DOF Z/W = 0.024 [V]
Jim W suggested that I run the script for the STS's as well while I'm here.
There are 1 STS proof masses out of range ( > 2.0 [V] )!
STS C DOF Z/W = 3.155 [V]
All other proof masses are within range ( < 2.0 [V] ):
STS A DOF X/U = -0.947 [V]
STS A DOF Y/V = 0.13 [V]
STS A DOF Z/W = -0.068 [V]
STS B DOF X/U = 0.886 [V]
STS B DOF Y/V = 0.62 [V]
STS B DOF Z/W = 0.563 [V]
STS C DOF X/U = -1.536 [V]
STS C DOF Y/V = -0.929 [V]
STS EX DOF X/U = 0.516 [V]
STS EX DOF Y/V = -1.076 [V]
STS EX DOF Z/W = 0.387 [V]
STS EY DOF X/U = 0.518 [V]
STS EY DOF Y/V = 0.683 [V]
STS EY DOF Z/W = -0.266 [V]
FAMIS #4366 closed
As part as Tuesday maintenance today March 8, 2016 CDS system admins will be deploying a new file system ( /Ligo ) the switch over will limit the ability to use any workstation or server that mounts /Ligo until the work is completed; Once the switch over on the MSR has been done, every workstation must be updated and restarted.
Sheila, Jenne, Matt, Rob, Evan, Lisa Several things happened today, more details will be posted later:
Higher-than-before jitter coupling seems to have made a lot of excess noise peaks. See these high coherence peaks between DARM and various IMC WFS signals (only WFS DC signals are shown).
It doesn't look like the intensity noise caused by the jitter (look at low coherence between DARM and ISS second loop signal, also IM4_TRANS_SUM coherence is low even when IM4_TRANS_PIT coherence is high).
Something seems to be excited on the PSL table (look at the coherence between DARM and PSL table accelerometer).
What happened in the PSL since Feb 26 2016 16:30 UTC when the IFO was in good low noise lock?
Lisa, Evan
We repeated the DARM-to-OMC coupling test (25852) at full power.
Tentatively, the change in the violin mode heights with the OMC locked and unlocked suggests only a 75 % coupling into the OMC (i.e., a 25 % loss).
We are not sure why the violin mode at 502.8 Hz is fatter with the OMC locked, so we would like to repeat this test with a calibration line.
This 502.8Hz mode seems one of the violin mode for ITMX, accoding to the wiki https://awiki.ligo-wa.caltech.edu/aLIGO/H1%20Violin%20Mode
If that's true, just to be sure, you should use one of the ETM violin modes, or ETM cal line as you mentioned.
When I was doing a beacon scan using some of the violin modes, I found that the 45MHz modulation sidebands also had finite response to the violin modes.
Assuming this came from the motion of the ITMs, I learned that I needed to use the ETM motions in order to correctly figure out the signal mode matching.
I made a quick "noise budget" which accounts for most of the H1 noise with just shot noise, coating thermal noise, a 1/f mystery noise, and a 1/f^4 "other noises" curve. This is a much poorer version of the real noise budget, but it is enough to help with the mystery noise search.
State of H1: locking well, and made it to Low Noise multiple times
Commissioning:
Site activities:
Current Status:
Even if H1 had been brought back to low noise before the week-end, the SensMon was not properly showing the range. This was due to a change in the whitening filters in CAL_DELTAL_EXTERNAL_DQ that happened last week (see Sheila's entry ). John Z updated SensMon to take the new filters into account (thanks John), so the range monitor is back, and the summary pages show it correctly.
WP 5765 See T1600062 for details of all updates.
SVN UP'd:
hugh.radkins@operator3:models 0$ svn up
U isi2stagemaster.mdl
A ISI_to_SUS_library.mdl
Updated to revision 12797.
hugh.radkins@operator3:models 0$ pwd
/opt/rtcds/userapps/release/isi/common/models
hugh.radkins@operator3:src 0$ pwd
/opt/rtcds/userapps/release/isi/common/src
hugh.radkins@operator3:src 0$ svn up
A WD_SATCOUNT_vb.c
Updated to revision 12797.
Top Level Model edits:
Added Paths to all BSC top level models to calculate the SUSPOINT motion in the ISI. Once these are working in the ISI model, the calc done in the SUS model and the IPC to the SUS will be removed. See the attached for a before (left) and after (right) look at the model changes.
This morning we had a combination of moderately high winds (gusts up tp 30-35 mph) and microseism above the 90% percentile, this is a combination of ground motion conditions where we had trouble durring O1.
We attempted to lock several times, and probably would have been able to if we had just kept trying, although we had random locklosses at diffrent stages of the CARM offset reduction.
One thing that we know is a weak point in our acquisition now is the ALS DIFF loop, so Matt and I had a look at improving that loop. We saw that our UIM control filter, which has some modest plant inversion to make the crossover between the ESD and UIM stable, was not quite right. We had features just above 2 Hz which were causing us to nearly have a second UGF there, and gain peaking was clearly visible in our control signals. This was predicted by the sus model and our filters, although reality was a little worse than what was predicted.
The first attached screnshot is the OLG before (blue) and after (red). You can see that there was a small dip that nearly had multiple ugfs just above 2 Hz, which is improved a little. THe second screenshot shows the crossover measured by injecting at L1, the third one shows the change to the filter.
With this filter, we were no longer able to engage the 1 Hz resonant gain in the DARM filter bank. From our model it isn't clear why that would be, but we also don't see any reason why we need such an aggressive ResG at the moment, so we are leaving it out.
1/2 open LLCV bypass valve, and the exhaust bypass valve fully open.
Flow was noted after 95 seconds, closed LLCV valve, and 3 minutes later the exhaust bypass valve was closed.
Next over-fill on Thursday, March 9th before 23:59 utc.
It turned out that all my previous analysis did not correct for the time-varying optical gain when calibrating the cross spectra into displacement even though I thought I have done it. I have recalibrated all the O1 data with the optical gain properly corrected.
Fortunately, the conclusions I have arrived so far qualitatively did not change.
Here are some plots with the newly calibrated cross spectra, mainly to show there is no drastic changes.
Fig.1 Band limited rms of the cross spectra in time series for the entireO1 run. The old data (without the optical gain correction) are show as "+" symbols while the recalibrated data are shown as dots.
Fig.2 Ratio of the band limited rms, (new data) / (old data). Notice that the high frequency bands (bands 3-8) tend to have larger displacement now. The low frequencies do not fluctuate as big as those for high frequencies as expected.
Fig.3 A naive correlation diagram in which the linear dependency between high frequency bands (bands 5-8) is still visible.
Fig.4 Time series plot of scaled band 8 BLRMS, LVEA temperature and scaled vertical sensors of various suspended optics.
A report on correlation with the optical gain.
It seems that the overall behavior of the optical gain shows correlation with the band limited rms. Is this calibration artefacts or something real ??
Darkhan provided me with kappa_c which was averaged over every 128 sec. In order for us to become less sensitive to glitches or some discontinuity in the Pcal line, we used kappa_c from the C02 frame that are smoothed by a median filter. In the second figure, I overlaid the old rms data which I did not correct for kappa_c by accident (as described in the above entry). Both corrected and uncorrected rms show somewhat good correlation with the rms.
The attached is the DARM model that I have used for calibrating the cross spectra. OLGTF = sensing * (atst + apum ) * userd.