Finished the alignment work with the ASAIR beam on ISCT6. The periscope had to be moved and the top mirror lowered. This allowed the beam to travel down periscope and hit the 2 steering mirrors on the table. Couldn't find a camera, so the beam is currently dumped.
Also installed the tube that connects the viewport adapter to ISCT6 and removed the Lexan protectors.
The feet of ISCT6 have been set down. The new table position still needs to be marked on the floor.
Images I took yesterday show that the 2nd reflection from IO_MB_L1 is clipping on the output aperture of the EOM. The beam is clearly seen on the housing on the +Y side of the output aperture. The beam should be going cleanly back through the EOM and be easily identified and dumped on or near the EOM steering mirror mount, such that there's no possible path for the beam to re-enter the optical system. The images also show that the beam is not centered on IO_MB_L2, and should be centered, and the beam is currently mis-centered to the -Y side of the lens. Both the clipping and mis-alignment show that the beam line from the EOM through the IMC mode matching lenses has not been restored to an alignment that satisfies the original design of the optical system.
Attached is document, T1800243-v1, that shows my IR images taken yesterday.
Being mi-centered through the IMC mode matching lenses has the potential to modify the shape of the IMC input beam, as well as increasing the effects of any small beam mis-alignment through the lenses, compared to having the beam better centered.
[Marie, Aidan, Alexei, Dan]
Summary
Yesterday we improved the LED return beam from the ETM to the point at which we could attempt to characterize the noise of the Hartmann sensor and run a measurement of the ring-heater. This was predominantly achieved by (a) improving the mode-matching of the LED beam to the in-vacuum optics and (b) imaging of the ETM.
Details
Our first approach yesterday was to try optimize the imaging of the ETM on the HWS camera. This was attempted using the usual method of injecting a YAW oscillation (10urad amplitude, 0.03Hz period) into the ETM and monitoring the centroid of the return beam on the Hartmann sensor. The amplitude of the oscillation on the centroid should go to zero when the Hartmann sensor is at the conjugate plane of the ETM. However, we moved the Hartmann sensor longitudinally over a range of approximately 30cm and saw no noticeable change in the amplitude (which remained at 10 pixels, or 20 pixel pk-pk) on the Hartmann sensor.
Additionally, we measured the distances (as best we could) between the various optics in the Hartmann sensor path. The results are:
| Parameter | Measurement | Design [T1000717] |
| Source to Lens 1 | 0.762 m (+/- 5mm)* | 0.9036m |
| Lens 1 focal length | -0.5589m (specification) | -0.5589m |
| Lens 2 to Lens 2 | 1.0858m (+/- 5mm) | 1.079m |
| Lens 2 focal length | +2.2361m (specification) | +2.2361m |
| Lens 2 to Lens 3 | 0.6112m (+/- 5mm) | 0.610m |
| Lens 3 focal length | +2.2361m (specification) | +2.2361m |
* The distance from the Hartmann sensor to Lens 1 was estimated to be approximately 2"-4" shorter than this. Nominally, the source and the Hartmann sensor should be at the same distance from Lens 1.
The first take-away from this was the Hartmann sensor appeared to be approximately 20cm - 25cm too close to Lens 1.
The input beam from the LED source was approximated by a beam 4mm radius and converging to a focus 1.5m from the source, see TCS eLOG 210. Knowing this, we could inject this beam into a paraxial beam propagation of the full ETM/TMS system to estimate the beam size through the system. The remaining relevant parameters are reproduced here from T1000717-v5.
| Parameter | Value |
| Lens 1 to TMS secondary mirror T2 | 4314mm |
| Secondary mirror, T2 ROC | -200mm |
| Secondary mirror, T2 to Primary mirror, T1, distance | 1902.6mm |
| Primary mirror, T1 ROC | 4000 mm |
| T1 primary to ETM HR distance | 1429 mm |
| ETM ROC | -2245m |
| ETM ROC apparent (as viewed from outside)* | -1537m |
* Assuming n = 1.4607 for 532nm.
Beam propagation (with 1.5m convergence)
We propagated the nominal input beam (4mm radius, +1.5m focal point) through a paraxial beam propagation (it's not a remotely Gaussian beam) from the source through to the ETM and then back to the Hartmann sensor. The results are shown below. Inside the vacuum system, the optics are all (mostly?) 1" diameter on the TMS table. A 1" diameter optic at 45 degrees has a clear aperture horizontally of the order of 16mm across. So, the beam propagation is also shown with the scale limited to 8mm. This makes it very obvious that the return beam is likely significantly clipping horizontally on the TMS & in-air optics.

The return beam looked something like this:

Beam propagation (with 0.87m convergence) - improved mode-matching
I changed the input beam to 0.87m convergence. And the model suggested significant improvement in the nominal mode-matching. It suggests that the input and return beam are well balanced, that we have a good retro-reflection from the ETM HR surface and that we are not likely to be clipping on any of the 1" optics. The beam size is approximately a factor of 1.7x smaller than the limiting aperture size.

This change was facilitated by adding a 9mm spacer to move the 1" diameter, 125 mm focal length lens further from the 20 mm lens inside the fiber launcher.
Initial system: S_input - S_lens = S_output
S_input = S_output + S_lens = -1/1.5m + 1/0.125m = 7.33 diopters
Therefore input beam looks like it's coming from a point 1/S_input = 0.1363m behind lens
S_out_target = -1/0.87m
S_input_target = S_out_target + S_lens = -1/0.87m + 1/0.125m = 6.85 diopters
Therefore input beam needs to like it's coming from a point 1/S_input_target = 0.146m behind lens.
Therefore, we need to add another 9mm or 10mm spacer to move the lens forward.
We added a 9mm spacer.
Improved return beam
Following this we optimized the alignment of the return beam by eye, and also moved the Hartmann sensor back approximately 20cm to move it closer to the conjugate plane of the ETM HR surface.
The return beam started to look much cleaner. There is still some high spatial frequency noise on it and it looks like it might be clipping somewhat, but it now appears to show the 220mm diameter annular reaction mass hole. The beam was less elliptical and more circular (but not completely). We could also close the iris down in front of the fiber launcher and see a crisp circle of light on the Hartmann sensor (which we couldn't before).
The improved return beam looked like this. The magnification with the measured values is estimated to be 23.5x. I demagnified the annular reaction mass hole [D1500163] (diameter = 222.5mm) by 23.5x and drew it on the return beam (yellow line). I strongly suspect that the circular aperture in this image is the AERM hole.

Hartmann sensor measurements
Given that we were getting toward the end of the day, we decided to install the Hartmann plate and run the Hartmann sensor overnight. We initialized the code and saw approximately 300 spots - indicating good coverage. The spherical power seemed to fluctuate around +/- 4E-6 diopters. We also set up the ring-heater to run. We'll summarize these results in another aLOG.
In conclusion, there is definitely room to improve (a) the input beam size, (b) the mode-matching, (c) the alignment to the ETM and (d) the imaging onto the Hartmann sensor. However, these results are very encouraging.
The Hartmann sensor beam looks like this:

Sheila, Thomas, Jenne, Craig
We were able to lock PRMI this afternoon/evening, but we needed larger gains than expected. We will still need to spend some time with PRMI checking that phases, build ups and gains make sense.
Other details from today:
About the phase changes for 45MHz:
Jenne had adjusted phases using PRX on May 14th 41986, and found a phase shift of -40 degrees for 45MHz, while Thomas found -60 degrees using MICH last night. For 9 MHz, Jenne's PRX phase shift was +60 while our MICH phasing was +75 degrees. Some but not all of the phase shifts Jenne made on May 14th were lost in the model reboots on May 22nd.
Two points of confusion that can be cleared up by the table below. We moved the phase for REFL45 too far (we have added our phase shift on top of Jenne's), which might explain the low optical gain for MICH in PRMI. Jenne had phased REFL 9 but not POP9, which is why TVo found that POP9 needed a phase shift but not REFL9. This can't explain the low optical gain for PRCL.
| May 14th change | May22nd | May 23rd | ||
| POP45 | none | no change | -60 | |
| REFL45 | -36 | -40 | -100 | |
| POPAIR45 | none | none | -60 | |
| REFLAIR45 | no net change | none | -60 | |
| REFLAIR135 | none | none | +180 | |
| POP90 | none | none | -120 | |
| ASC ASA+B45 | -40 | reset to 0 | -60 | |
| ASC REFLA+B45 | -40 | rest to 0 | -60 | |
| ASC POPX RF | -40 | reset to 0 | -60 | |
| POP9 | none | none | +75 | |
| REFL9 | +60 | +59 | +59 | |
| POPAIR 9 | none | none | none | |
| REFLAIR 9 | none | none | none | |
| REFLAIR 27 | none | none | none | |
| pop 18 | none | none | +146 | |
| ASC REFL A+B | +60 | reset to 0 | none | |
| AS A+B 36 | none | none | none |
Gerardo M., Kyle R.
The modified annulus piping was finished being installed on GV11 today. The new arrangement eliminated some unneeded joints and lengths (runs) of piping and now everything is much "tidier". As part of this exercise we vented the gate annulus volume with UHP N2 and observed that neither the inner nor the outer gate O-rings leak now. Prior to baking CP4, both of GV11's gate O-rings leaked significantly, as well as, GV12's inner gate O-ring. The assumption being that the Viton had become less compliant after 20 years exposure to vacuum but must have softened after 8 weeks of being compressed and heated. We are pumping the annulus volume with a turbo overnight and will helium leak check tomorrow.
Next, we will repeat this exercise on GV12.
[ Alexei, Dan Brown ]
The jupyter notebook for all the relevant calculations is on the LIGO git.
I noticed an odd shape of the second order resonance (can be seen in single_fit.png) in the OMC scans related to the SR3 heater testing. This shape was very consistent between scans and only seemed to show up on the second order mode. Recent beam scan measurements [ alog 41683 ] have shown that the beam could be significantly astigmatic, thus influencing the shape of the second order resonance.
To test out the hypothesis I tried to fit two lorentzians to the second order peak (corresponding to the TEM02 and TEM20 modes).
The following model was considered
model = a1 * L(t,fwhm,t0-df) + a2 * L(t,fwhm,t0+df)
Where
L(x,fwhm,x0) = 1 / (2 * pi) * fwhm / ( (x-x0)^2 + (0.5 * fwhm)^2)
is the lorentzian function
The fit was performed by using Nelder-Mead to vary [ fwhm, a1, a2, t0, df ] to minimise [ sum(abs(data-model) ]. The resulting fit seems good as can be seen on double_fit.png and double_fit_residual.png.
The model returns the power of the second order modes as
P_20 = a1 * 2 / (pi * fwhm)
P_02 = a2 * 2 / (pi * fwhm)
Numerically the values are P_20 = 0.21 and P_02 = 0.09, which correspond to a mismatch of 13.7% [ using (P_20 + P_02) / P_00 ], where P_00 was measured separately as 2.17 from the same scan.
Note that the naive way of measuring mismatch [ P_2/P_00 ] gives 10.7% or 13.2% if the correction factor of 1.23 from [ alog 41679 ] is applied, where P_2 = 0.233 is the maximum value of the second order peak.
Using the expression for the power loss of due to mismatch from an astigmatic beam [Eq 21 in T1800165-v2 ] we get 13.9% of power loss.
The full description of the shape of the second order peak also has to include the contribution from the TEM_11 mode, which resonantes between the TEM_20 and TEM_02 modes. This can be modelled by adding
another lorentzian. The model is now
model = a1 * L(t,fwhm,t0-df) + a2 * L(t,fwhm,t0+df) + a3 * L(t,fwhm,t0)
Where Nelder-Mead tries to minimise the sum of the residual between the model and the data by varying [ fwhm, a1, a2, a3, t0, df ].
The resulting fit is only marginally better, which can be explained by the fact that the allignment loops for the OMC were closed (TEM_11 amplitude mostly couples through misalignments).
The resulting mode intensities are given by
P_20 = 0.199
P_02 = 0.0824
P_11 = 0.0252
The mismatches are
(P_20+P_02) / P_00 = 12.9%
1-sqrt( (1 - 2 * P_20 / P00) * (1 - 2 * P_02 / P00) ) = 13.0%
So accounting for the TEM_11 peak drops the mismatch by about 1%.
Special care has to be taken with the fitting as I've found the results can vary wildly depending on the minimizing routine used and the initial conditions of the fit. I don't have enough faith in these fitting algorithms for them to be able to
work robustly without oversight.
It looks like one can extract information about the astigmatism of the beam going into the OMC from OMC scans (contrary to what I may have claimed before) by carefully fitting lorentzians to the measured second order peak.
This may be useful in hunting down and remedying the unkown source of the astigmatism that has been plaguing us.
Sheila, TVo
We noticed that the boost filter would cause the IMC to oscillate so we checked the OLTF again and found the UGF at 4 kHz, so we added +15 db to the servo gain and found a new UGF of about 30 kHz. This is probably due to the new EOM changing the modulation depth.
This seems high. The modulation depth is estimated to be only 3 times lower.
Yeah it did seem odd, but we reduced the gain by 4db here previously. So in the end it's about +11db which is close to what we'd expect from the EOM swap, maybe.
ETMY HWS running tonight for noise measurements. RH coming on at 2W around 11:30PM tonight for 8 hours.
Full report tomorrow.
Betsy, Travis, Gabriele
This afternoon Gabriele was kind enough to help us take the in-air violin measurements on the ETMXQUAD sus. We set up all of the in-chamber equipment (HeNe laser/QPD setup) and adjusted them to sight across one fiber at a time, while Gabriele ran the spectrum analyzer.
We were able to obtain data from the first 3 harmonics of the v-modes on 2 of the fibers (took about 2 hours). Tomorrow we will proceed with the other 2 fibers. More to come...
WP 7592
Newly replaced PT110 Inficon Gauge BCG450 was found to have one set of faulty contacts. This is preventing the HV power supplies interlock from enabling and turning on the HAM6 HV power supplies. Faulty contacts were bypassed.
Also to note: I enabled and set the pressure/HV interlock CoE parameters for PT170 and PT110 to 1e-5. This had not been done when they were installed. Both are new BCG450 gauges.
ISCT6 enclosure was moved to final location, alog 42101. Cables had to be be redressed to clear one of the clean room legs. Two of the picomotor cables ISC_182 and ISC_183 were too short,cable extensions were added.
TITLE: 05/23 Day Shift: 15:00-23:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:
LOG:
15:14 APS on site
15:29 HFD on site for hydrant testing
15:30 Marc and Hugh out to vault/LVEA
15:35 Jeff B out to LVEA to investigate TCS water leak
15:54 Richard out to LVEA
16:01 Jason out to LVEA to investigate TCSY leak
16:20 Jason back
16:23 Karen servicing Y arm
16:24 Dan and Marie out to Squeezer Bay
16:25 Peter out to PSL enclosure
16:30 Richard back
16:35 Chandra into LVEA to valve in RGA
16:37 Fil out to LVEA for HAM6 cabling
16:38 Mark and Tyler to EX to remove arm from BSC
16:50 Jason out to PSL enclosure
16:51 Dan, Marie and Alexie out to EY
17:00 Chandra back
17:15 Aiden out to EY
17:53 Marc and Hugh back and done
17:56 Jeff B back
18:00 Jason and Peter back
18:24 Jeff B out to transition the LVEA to LASER hazard
18:30 Cheryl and Jeff J out to PSL enclosure
18:43 Travis to Optics lab
18:50 Travis out
20:59 Aiden, Aiden, Marie, and Alexie out to EY
21:25 Cheryl back
22:02 Jeff B out to HAM6 to reset dust monitor and mechanical room to check on TCSY chiller
22:09 Kyle and Gerardo to MY
22:12 Jeff B back
22:24 Marc to MX
22:25 Amber in CR with tour
22:27 Chandra out to MY
22:57 Marc back
Transfer functions of the ISS were made for various gain slider settings from 0 dB to 21 dB.
It was quite noticeable that once the gain was increased beyond 16 dB, the loop started
oscillating. However in the power noise spectra there are a number of features (spikes and
broad peaks) that were not present before. These are not caused by the noise eater as they
are present when the noise eater is on or off. The broad peaks are not present in the
spectrum when the light is blocked. So they may be caused by scattered light.
More measurements and characterisation is necessary.
Jason / Peter
Richard, Dave: Due to ongoing fire pump work, these alarms have been silenced to cell phones for the remainder of the afternoon.
Bypass will expire:
Wed May 23 17:41:13 PDT 2018
For channel(s):
H0:FMC-CS_FIRE_PUMP_1
H0:FMC-CS_FIRE_PUMP_2
bypass removed
J. Oberling, P. King
Today we worked on recovering the PSL ISS, and began by re-installing the ISS AOM. The AOM mount was moved to a place where the beam was ~1mm in diameter (unfortunately I forgot to take pictures, will take some tomorrow and upload as a comment) and installed the AOM. The mirror that sits downstream of the AOM and reflects the 1st order diffracted beam into a beam dump was also re-installed and aligned. A power meter was placed in this beam path and the alignment of the AOM tweaked to maximize the power in the 1st order beam. We then adjusted the ISS offset to find the point where the AOM was diffracting ~2W; this was found at an offset of 8.0. The offset was then set to 0, and increased to 20 in steps of 1; a power reading for the 1st order beam was taken at each step. This allows for calibration of the diffracted power graph on the ISS MEDM screen. Peter has the data and is analyzing it.
The beam from the PMC to the ISS box had to be re-aligned, as we had not re-aligned this path since moving the ISS box to accommodate the damping bars for the new PMC. This complete, we then roughly aligned ISS PDB. The PD assembly was then removed from the ISS box so we could re-install ISS PDA (recall that PDA had been removed from the ISS box and installed in place of IO_AB_PD3 prior to O2). With PDA back on the PD assembly, this was installed back in the ISS box, and both PDs aligned. They both now read ~10.0 V. Next step on the ISS (for tomorrow) is to get the loop to close and measure TFs to optimize its operation.
Attached is the calculated fit to the percent diffracted power versus offset slider setting.
Ihe fit is close to a parabola p(x) = 113.18 x^2 - 82.3309 x + 15.0625.
The power measured in front of the AOM was 67.8 W, and after the neoVAN amplifier was
69.8 W. The power in front of the AOM was used in calculating the percentage diffraction.
I went ahead and changed the coefficients in the ISS MEDM screen that calculates the percentage diffraction.
Set the reference level to be -1.89 and closed the loop without any problems.
The offset slider is currently set to 8.00. Please do not mess with this value. Only the reference level
(labelled REFSIGNAL) and the gain slider should be adjusted. At the time of making this log entry the gain
setting has not been determined as that will require a few transfer function and noise measurements.
The promised pictures. The 1st is the ISS AOM installed in its new location. The 2nd is the mirror that directs the 1st order diffracted beam from the AOM into a beam dump (bottom-left of picture); the power meter shown was used for alignment of the AOM.
Filiberto C., Daniel S., Marc P.
Today we successfully applied E1600252v2 to the OMC DCPD ISC Split Whitening Chassis S1101627. This change better accommodates the violin modes of the main LIGO optics in the vicinity of 500Hz that have a tendency to saturate the whitening chain's filters. The new filter replaces a 1Hz-10Hz zero-pole, with a 50Hz-500Hz pole-zero on the second filter channel. LLO had already completed these changes August 2016, ALOG.
Updated the DCPD whitening filter at stage 2 to a nominal zpk([50],[504],-1, "n"), ie., zero at 50 Hz, pole at 504 Hz, gain of -1. This may effect the calibration.
Found a GigE camera (MAC: 00:30:53:22:94:A0) in the squeezer bay and mounted it in the ASAIR beam on ISCT6.
Reconnected the picomotors for HAM6.