Evan, Yuta, Kiwamu,
Commissioning of the dithering system is underway.
A summary of the red commissioning from this morning:
(Alexa, Jeff)
The IMC-X_M1 and IMC-X_M2 wresg calibration filters are off by a minus sign. I have attached the plots depicted in foton and those produced by Jeff's model. The phase is 180 deg in foton, but should be 0 at DC. I have not updated foton, but an email has been sent out to the relevant parties.
The BSC-ISI watchdog plotting software was reported disfunctional by Hugh earlier this week.
I looked into the scripts and they were fine. What I had missed is that Charles had updated the BSC-ISI WD screens, wich thus needed to receive an svn up at the site to match the latest wd_plotting software update, performed when updating the HAM-ISI models last week.
I run the the svn up on: /opt/rtcs/userapps/release/isi/common/medm/ISI_CUST_CHAMBER_WATCHDOg.adl remotely.
The WD plotting software now works on all the SEI platforms of H1.
HAM2 and HAM3 as well as the HEPIs tripped at the exact same time (actuator trip for all of them) @ gps 1077061619 (15:46 PT)
It happened again this evening when Sheila restarted the Beckhoff at 1077078129. HAM2 and HAM3 ISI actuactors tripped because of a spike in the act signal, as well as the HEPI. cf attached plots
Jamie and I tried this a few more times..
Stoping and restarting the EPICs database doesn't unlock the IMC.
Stoping PLC2 does unlok the IMC (and FSS) , although in the three times I tried it it didn't trip any HAMs today. Restarting the other PLCs doesn't cause any problems, and it doesn't matter wether or not the Guardian is running.
15:47 DAQ Restart. Support of h1lsc model change.
As requested by the green team, I edited the LSC model which now allows one to route the LSC sensor signals to the DAC through ALS_C_REFL_DC_BIAS.
Tested the dust monitors at End-Y. Found dust monitor #2 (in the test stand cleanroom) was not working. I moved dust monitor #1 (from the spool area cleanroom) to under the test stand, and verify its operation. Dust monitor #2 has been returned to Richard.
Seems like it was yesterday's burt-restoring to a bad time for ALS WFS. Manually restored them.
At 14:25:00 and 14:26:00 a signal was injected into the seismometer channels for H1:PEM-MX to test a suspected delay in signals showing up in dataviewer displays in the control room. There was no delay. Signal was injected by striking the floor of the VEA with a heavy plastic mallet. There is a time conversion issue on playback in dataviewer in which the UTC time entered is not the time that gets played back, but if GPS time is used, it is correct. This will be investigated and corrected.
Except for Corey doing some last moment inventorying, the Cartridge is ready for install. The Test Stand is stripped of all field cables, in-vac cables are all tucked away, accessible areas of the ISI were wiped down (not too much collected it seemed,) and covers are on ready to drop around Stage0 when the assembly lifts from the Stand. No incumberances seen at this time.
Thanks to Betsy & Mitchell.
Keita is getting started with green WFS, so we are doing the strait shot alignment first.
Baffle PD 1: PIT 221.0 YAW -228.1, saved using the new guardian state
Baffle PD4 PIT 290.6 YAW -289.8 saved as well
Alinged: 255.8PIT -259 YAW saved as Alinged
I didn't move PR3 since the spot already looks centered on the camera: -244 PIT -254 YAW
Installed DustMonitor 12 in clean room over Ham5. Alarm levels are set high at the moment as the chambers are closed.
Cleaned the lens and repositioned the camera. Zoomed in and focused on the ITM. We can see PRMI spot on optic. Someone may want to make more adjustments. The camera view is probably upside down.
This completes dewar vacuum jacket pumping exercise. Summary below: 8514374 As found = 780 microns -> As left on 12/20/2013 TC = 4 microns, Pirani = 1.5 x 10-3 torr, 8514372 As found = 28 microns -> As left on 1/23/2014 TC = 4 microns, Pirani = 1.4 x 10-3 torr, 8514371 As found = 61 microns -> As left on 1/27/2014 TC = 7 microns, Pirani = 1.6 x 10-3 torr, 8514375 As found = 45 microns -> As left on 1/31/2014 TC = 6 microns, Pirani = ? torr, 8514376 As found = 49 microns -> As left on 2/4/2014 TC = 6 microns, Pirani = 1.7 x 10-3 torr, 8514377 As found = 42 microns -> As left on 2/7/2014 TC = 6 microns, Pirani = 1.8 x 10-3 torr, 8514379 As found = 81 microns -> As left on 2/13/2014 TC = 6 microns, Pirani = 2.0 x 10-3 torr, 8514380 As found = 58 microns -> As left on 2/21/2014 TC = 7 microns, Pirani = 1.8 x 10-3 torr.
----------Morning Activities---------
Dave B., Patrick T. Just realized that the system time for h1conlog is ~ 1 min 42 sec in the future. NTP needs to be set up. We will do this during Tuesday maintenance. We also added three channels for testing: H1:PEM-CS_GDS_0_RSET H1:PEM-CS_GDS_0_SW1 H1:PEM-CS_GDS_0_SW2
(Jax, Keita)
Yesterday morning we measured the sensing matrix for the ALS WFS. We did this by Injecting 30000cts at 5Hz into H1:SUS-L2_(I/E)TMX_L2_TEST_(P/Y)_EXC, then measuring the transfer function between H1:ALS-X_WFS_(A/B)_I_(PIT/YAW)_OUT and H1:SUS-(I/E)TMX_L3_OPLEV_(PIT/YAW)_OUT.
In cavity basis:
Pitch Sensing Matrix: (WFS ct/uRad)
Hard | Soft | |
A | -24871 | -44392 |
B | -10475 | 52694 |
Pitch Input Matrix: (uRad/WFS ct)
Hard | Soft | |
A | -2.967e-5 | -2.5e-5 |
B | -5.899e-6 | -1.401e-5 |
Pitch Output Matrix:
0.707 | 0.707 |
-0.707 | 0.707 |
Yaw Sensing Matrix: (WFS ct/uRad)
Hard | Soft | |
A | 38421 | 67629 |
B | -18263 | -25945 |
Yaw Input Matrix: (uRad/WFS ct)
Hard | Soft | |
A | -1.088e-4 | -2.838e-4 |
B | 7.665e-5 | 1.612e-4 |
Yaw Output Matrix:
0.707 | 0.707 |
0.707 | -0.707 |
Raw data:
Useful information for determining sign conventions from raw data:
1. ETM/ITM Yaw is defined with positive as a counter-clockwise rotation of the optic around the z-axis.
2. ETM/ITM pitch is defined as positive pitch "down", but ITM oplev is set such that an increase in pitch gives a decrease in oplev measurement.
ETM Yaw:
WFS | dB Magnitude | Phase |
A | 86.3 | 126 |
B | 74.7 | -46.1 |
ETM Pitch:
WFS | dB Magnitude | Phase |
A | 93.79 | 123.2 |
B | 89.5 | -57.8 |
ITM Yaw:
WFS | dB Magnitude | Phase |
A | 97.5 | -62.58 |
B | 89.9 | 122.24 |
ITM Pitch:
WFS | dB Magnitude | Phase |
A | 82.8 | 115.7 |
B | 93.0 | -60.7 |
Edited the main alog to make some of the definitions more clear and add the calculated output matrices.
The input/output matrices have been added to the computer system:
H1:ALS-X_WFS_INPIT_MTRX_...
channel | value |
1_1 | -0.00003 |
1_2 | -0.00003 |
2_1 | -0.00001 |
2_2 | -0.00001 |
H1:ALS-X_WFS_INYAW_MTRX_...
channel | value |
1_1 | -0.00011 |
1_2 | -0.00028 |
2_1 | 0.00008 |
2_2 | 0.00016 |
H1:ASC-OUTMATRIX_P_...
channel | value |
5_17 | 0.70711 |
5_18 | 0.70711 |
7_17 | -0.70711 |
7_18 | 0.70711 |
H1:ASC-OUTMATRIX_Y_...
channel | value |
5_17 | 0.70711 |
5_18 | 0.70711 |
7_17 | 0.70711 |
7_18 | -0.70711 |
Written by Yuta
From the measured WFS sensing matrix, the estimated Gouy phase difference between WFSA and WFSB is 66 +/- 4 deg for pitch and 24 +/- 5 deg for yaw.
I think this is a reasonable measurement. See also alog #10056.
[Method]
Theoretical WFS sensing matrix can be written as;
DIFF COMM
WFSA P*(a*sin(etaA)-b*cos(etaA)) P*(c*sin(etaA)-d*cos(etaA))
WFSB P*(a*sin(etaB)-b*cos(etaB)) P*(c*sin(etaB)-d*cos(etaB))
a,b,c,d can be calculated by the cavity geometrical parameters(length, RoCs). So, from the sensing matrix measurement, P, etaA, etaB can be estimated by the fitting.
Here, I used the least squares method (scipy.optimize.leastsq) to estimate etaA and etaB, and the measurement error is assumed to be 10% for all the sensing matrix element.
[Result]
Attached. Curves show theoretical WFS signal dependence on the Gouy phase. DIFF and COMM is approximately HARD and SOFT mode of the caivty.
(Comment added: HARD/SOFT is opposite in the measurement?)
[Evan, Paul]
Here is a summary of the analysis of beam size measurements reported in 9898 and previous, in context with expected parameters from a model of the PRMI.
The first attached plot shows the ITMX direct reflection : PRM direct reflection beam size ratios predicted at the ISCT1 measurement location, as a function of ITMX susbtrate lens and PR2-PR3 distance offset*. The diagonal lines on the plots indicate the measured value of this beam size ratio**. There are also 3 pairs of red and blue vertical lines on the plots. The blue lines represent "cold states" and the red lines represent the designed for "warm state" with a +50km (+20uD) thermal lens in the ITM. The left-most pair of blue and red lines corresponds to the "expected" ITM lens state: -80km (-12.5uD) non-thermal lens in the ITMX substrate. The middle pair of blue and red lines corresponds to the "design" ITM lens state: no non-thermal lens in the ITMX susbtrate. The right-hand pair of blue and red lines corresponds to the "estimated" ITMX lens state, given the assumption that the generalized PRC parameter 2*PR2->PR3 - PR3Rc is as designed.
By assuming PR2-PR3 is as designed, we can estimate an ITMX non-thermal lens of +15uD (6.7km). The estimate from x-axis data and y-axis data agrees very well here. By assuming that the ITMX non-thermal lens is the -12.5uD (-80km) that came from surface figure measurements, we can estimate that the PR2-PR3 offset is +8.82mm. However, it should be noted that other simulation results showed that PRY is very likely to be unstable for such a large PR2-PR3 offset. As far as I'm aware, this was not observed during PRMI commissioning, though I'd appreciate some confirmation if anyone has any. Of course, any combination of PR2-PR3 offset and ITMX lens deviation that gives beam size ratios along the diagonal line is not discounted by these measurements.
The second attaced plots shows the same data for the ITMY measurements, which were taken while 4W was being applied to the ITMY ring heater. For ITMY we have no prior information about the non-thermal substrate lens, so the blue and red lines are not added. The only sensible prior information to assume, just for comparison, is that the non-thermal substrate lens is 0uD (+inf km). This is the right hand edge of the plot. The black dashed line represents the expected substrate lens caused by 4W of heating with the ring heater, using Aidan's number of -13.6uD/W. The diagonal lines again represent the measured beam size ratios. This seems to suggest that the non-thermal substrate lens is around +32uD (31.25km) in the x-axis and +40uD (25km) in the y-axis, again under the assumption that PR2-PR3 distance is as designed. From the ITMX plot and the ITMY plot, we should at least be able to pin down the difference in non-thermal lens power between ITMX and ITMY, even if we can't pin them down individually.
Next, I wanted to take a look at the consequences for actual mode matching in the interferometer, specifically between the IMC and PRX, PRX and XARM.
The third and fourth attached plots shows the IMC-PRX eigenmode overlap and PRX-XARM overlaps respectively over a slightly larger xaxis-range than for the first attached plot, but with the same blue and red lines for ITMX susbtrate lenses. Both diagonal lines from the plots in the first attached figure are included on these mode overlap plots: it is clear that lines from x and y-axes lie very close to each other. The important thing here is that at the "estimated" ITMX non-thermal lens value +15uD and the as-designed PR2-PR3 length, the IMC-PRX overlap is 99.5%(x) and 98.5%(y), and the PRX-XARM overlap is 99.7%(x) and 99.2%(y). If we allow for a +20uD (+50km) thermal lens on top of this value, these overlaps change to IMC-PRX 99.4%(x) 99.8%(y) and PRX-XARM 99.8%(x) 100%(y). In short: IMC-PRX and PRX-XARM should be mode matched well at cold and warm states if we believe the beam size measurements. Of course, the mode matching starts to suffer at a bit lower power than planned as a result of this, but PRX-XARM should still remain >97% for effectively all powers up to 125W. Also worth noting here is that for the mode matching, it doesn't matter right now whether it's the PR2-PR3 length that is off or the ITM non-thermal lens power, since the slope of the mode overlaps with respect to PR2-PR3 offset matches the diagonal lines from the beam size measurements.
I've also been looking at PRX-PRY overlaps for comparison with PRC gain observations as a function of ring heater power, but this post is already too long so I'll post that later.
* PR2-PR3 was varied in the simulation, but for these purposes it's degenerate with PR3 Rc change. The actual quantity that seems to matter most is (2 x PR2-PR3 distance - PR3 Rc), but in the simulation it suffices to vary just one of these. In practice we can only change PR2-PR3 distance so I plot that one.
**One caveat there: since the x-axis PRM measurement is believed to have been affected by the reflection from the back surface of the pick off window, I used the the model value of PRM direct reflected beam size and the measured value of the ITMX direct reflected beam size for computing the ratio. For comparison, the y-axis PRM direct reflected beam size (unaffected by the second reflection form the window) was measured to be 2.15mm, compared to the model value of 2.138mm. This is less than 1% difference, and the PRM model x-axis beam size was scaled by 2.15/2.138 to account for the possible small error in measurement location.
And here is the result of some more modeling for the PRX/PRY overlap, as a function of applied power to the ITMY ring heater (using -13.6uD/W) and PR2-PR3 offset. The first attached plot is for a constant ITMX non-thermal lens of -12.5uD (-80km), and the second attached plot is for a constant ITMX non-thermal lens of +14.6uD (+68km).
Firstly, the predicted required ITMY RH heating for PRX/PRY matching in the -80km ITMX lens case is 9.5W, whereas the required heating for the +68km ITMX lens case is only 7.5W. This might be a clear enough difference in optimal heating power to observe experimentally. This value is also independent of PR2-PR3 offset*.
Secondly, the difference in PRX/PRY overlap between cold state and optimally matched state for the the -80km ITMX is 60% (from ~40% @ 0W ITMY RH to 100% @ 9.5W ITMY RH), compared to 29% (from ~71% @ 0W ITMY RH to 100% @ 7.5W ITMY RH). I still need to convert this to PRC sideband buildup and POP18 signal for comparison with experimental data, but the differences look big enough to be apparent in the real PRMI.
Two caveats:
1. We don't know much about the non-thermal substrate lens in ITMY still, and this has a degenerate effect with the ITMX non-thermal substrate lens in terms of PRX/PRY matching. From the power required to match PRX/PRY we can really only extract information about the difference between ITMY/ITMX non-thermal substrate lenses (again).
2. Clipping at the BS can really be an issue here. As shown in LIGO-T1300954, this can make a big difference to the maximum PRC gain as well as the ring heater power at which that maximum gain is reached. This might actually give us another handle on the problem though: from the maximum PRC gain we may be able to estimate the clipping, thus beam sizes at the BS, and hence the PRC mode. Tricky with only sideband locks and no AS port, but maybe worth considering.
* Assuming no clipping at the beam-splitter...
Sheila, Alexa
After spending the afternoon on the arm locking, we spent some time looking at the COMM handoff. (Plots coming in the morning...)
I am leaving the arm cavity locking, PRM parked and ITMY misalinged, and the alingment servos off.
Here are some of the plots Sheila was referring to..
With the COMM PLL Gain at 19dB, we adjusted the CM Board Input 1 gain and looked at the amplitude spectrum from output 2 (i.e. the common path with the handoff engaged). We have data for a gain of 9dB, 12dB, 15dB, 18dB, and 21dB. These are plotted in Comm_Path_NoiseSpec.pdf.
I have also attached a GIF of the common path TF with the UGF at 3.9kHz, and 16kHz as we increased the gain.
In the first GIF that Alexa posted the reference trace is PLL gain 31, CM board IN1 gain 15. In the active trace the PLL gain has been turned down.
These plots show that we could push the bandwidth up to 35 kHz if we wanted to.
The BS IS tripped on GS-13 watchdog at 1328 utc this morning. Traffic, wind, something--plotting scripts still not functioning...
Anyway, I brought it back to lvl2 with 750mHz blends on stage2 and T250s on all Stage1 blends except T100mHz_0.44 blends on X & Y dofs.
I reset the target positions, there was about 700nrads on RX and <4um on Z, all other shifts were less. Please let us know if this impacts any alignments. This allowed for a one button isolation.
I reported the WD plotting issue mentioned by hugh last week. Details can be found in LHO aLog #10057
I am not sure what is going on yet, scripting or server access issue, but I am looking into it.
The plotting scripts work for the HAM-ISI. WD plotting is still disfunctional on the BSC. I think it is a scripting issue in that case, and I am working towards fixing it:
The BSC-ISI WD plotting software was fixed, see LHO aLog #10258 for more details.