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Section: H1
Task: INS
B. Weaver, J. Kissel WP 12109 Betsy, myself, and several others are looking to propose redlines to the WHAM3 flange cable layout (D1002874) in prep for O5 (see T2400150 for DCN and discussion there-of). However, in doing so, we discovered that the flange layout may have double-counted the shared cable for the MC2/PR2 M1 (top) RTSD / T1T2 OSEMs. Other drawings (e.g. the Cable Routing D1101463 and the wiring diagrams D1000599) indicate "yes, there's an extra 'SUS-TRIPLE' entry somewhere between the D6 and D3 allocation," but we wanted to be sure. As such, Betsy went out to HAM3 today and confirmed that YES the MC2/PR2 M1 (top) RTSD / T1T2 cable, labeled "SUS_HAM3_002" in the wiring diagram or "SUS-HAM3-2" in real life, does come out of D3-1C1 and *not* out of any D6 port, and thus we validate that D6's list of 4x DB25s to support the 'SUS-TRIPLE' (i.e. MC2) in D1002874 is incorrect. Pictures attached show the D3 flange, and highlight the SUS-HAM3-2 cable at the flange going to D3-1C1, and then the other end of that cable, clearly going into the MC2-TOP/PR2-TOP satamp box in the SUS-R2 field rack (S1301887).
J. Kissel, S. Koehlenbeck, M. Robinson, J. Warner The LHO install team (Jim, Mitch) -- who has experience installing in-chamber fiber optic systems -- have reviewed the two options put forth by the SPI team for optical fiber routing from some feedthrus to the future location of the SPI follower breadboard on the -X side wall of the HAM3 ISI using Eddie's mock-ups in D2400103. Both options (WHAM-D8 or WHAM-D5) are "evil" in several (but different) ways but we think the lesser of the two is running the fibers from D5 (the currently blank flange underneath the input arm beam tube on the -X side of HAM3; see D1002874). In support of this path forward, one of the primary evils with D5 is that access to it is *very* crowded with HEPI hydraulics piping, cable trays, and various other stuff. Here I post some pictures of the situation. Images 5645, 5646, 5647, 5648, 5649, 5650, 5651 show various views looking at HAM3 D5. Images 5652, 5653, 5654 show the HAM2 optical lever (oplev) transceiver, which is a part of the officially defunct HAM Table Oplev system which -- if removed -- would help clear a major access interference point.
I tested again the OMC aligment with low frequency lines, as in 76335
It looks like there is still some modulation of the DARM line amplitude at 410.x Hz. There is also some effect on the pitch jitter line amplitude, but no effect on the yaw jitter line amplitude.
New offsets that simultaneously make the DARM calibration line maximum and the pitch jitter minimum:
Old | Diff | New | |
---|---|---|---|
A PIT | -0.25 | -0.07 | -0.32 |
A YAW | 0.1 | 0.1 | 0.2 |
B PIT | -0.05 | -0.05 | -0.1 |
B YAW | 0.07 | -0.01 | -0.03 |
I put those offsets in. The range dropped. So they are not good. I don't understand why. I reverted them. The range went back. A step in the other directions did not change the range much, but KAPPAC dropped.
I checked that indeed GDS-CALIB_STRAIN was worse with the alignment offsets that made the range lower
Disregard the previous plot, there were two glitches in the data. DARM is slightly worse, but as significantly as thought.
Very low frequency angular lines are being injected in the OMC ASC controls starting at 14:39 UTC. The longer they run the better, but please feel free to stop them if other tests are ongoing.
awggui's are running on cdsws26.
This is a test to see if we can find a better OMC alignment position, and if this has any effect on DARM noise.
We reduced the amplitude by half at around 15:12:50 UTC, because this was saturating the OMC.
We paused these at 15:28:00UTC.
Earlier today I did some 2.6 Hz sine injection in DHARD_Y (71590) to understand the upconversion phenomenon seen previously (71505). This is maybe related to the non-stationary noise in the 20-50 Hz (71092) and the observed bicoherence (71005).
In summary: DARM noise between 20 and 80 Hz gets worse for positive excursions of DHARD_Y_IN1 from zero, but not for negative excursions.
It doesn't look like it is necessaarily correlated with the 2.6 Hz peak (although that peak contains a lot of the RMS in normal conditions).
This might indicate that we have a static offset in DHARD_Y alignment.
The first atttached spectrogram shows in the top panel a DARM spectrogram, whitened to the median of a quiet time, so that a value of 1 means normal noise levels. The bottom panel shows the DHARD_Y 2.6 Hz excitation amplitude, and the DHARD_Y error signal value. The most interesting feature is that noise in DARM is higher when DHARD_Y value is positive and large, but not when it is large and negative. The second plot shows a zoom in time of the same spectrogram, which makes the correlation evident.
To better understand, I computed the DARM BLRMS in the 20 to 50 Hz region [using the spectrogram, averaged over 2-s-long windows with 1-s overlap] , and compared it with the maximum value of DHARD_Y [in the corresponding 1-s window]. The third plot shows the corrrelation and the fourth plot is a time zoom showing the clear correlation with the positive peak value of DHARD_Y.
There is a clear correlation between the DARM BLRMS between 20 and 50 Hz and the maximum positive value of DHARD_Y_IN1, but not the maximum negative value. The last plot shows how the BLRMS is correlated with large positive excursions of DHARD_Y.
Possible causes for this behavior:
Some next useful tests:
As a side note, the RMS of DHARD_Y is dominated by a 1.3 Hz and a 2.6 Hz peaks. The 2.6 Hz peak could be the high frequency plant resonance, but the lowest plant resonance is at 1.05 Hz (71489). Previously I showed that there is some evvidence that the test mass M0 damping could be responsible for most of the DHARD_Y motion below a few Hz (71466). So maybe another useful test would be to check the status of the test mass M0 damping, and do some noise injections to properly project the OSEM noise contribution to DHARD_Y
On Saturday, while damping violin modes, I repeated this test, adding an offset to the DHARD_Y error point. The results are different than before: it looks like DARM is more noisy for negative excursions of the error signal from zero, instead of positive excursions as observed before. It appears that adding an offset that makes the error signal positive reduces the non-stationary noise in DARM.
It's not clear to me why this behavior is now different. Two ideas: 1) there are ASC error point offsets that change from lock to lock 2) this test was performed while dampiing violin modes, with a IFO still warming up, while the previous test was with a thermalized IFO
Some details.
Grounding.
I and Jim checked the ground loop for everything on A6 flange (ISC) again. I disconnected in-air cables from the feedthrough, put a DB25 breakout board on the feedthrough and tested the connection between pin13 (in-chamber shield) and the chamber ground.
The only genuine problem we found and fixed was a ground loop for ASC-AS_C QPD cable. Jim rerouted that cable that was bunched up under the ISI and it was fixed.
Also, when testing ground check for F1(OMC DCPD)/F2(OMC PZT)/F3(OMC QPD), disconnecting these three isn't enough. Don't forget to disconnect 3MHz cables (D4-2B1 and D4-2B2), otherwise there's this path which gives you anything from a few hundred kOhm to 4MOhm. We wasted some time because of this.
F1 in-chamber shield <-> DCPD preamp signal ground <-> RF cable SMA shield <-> SMA Rack ground -> chamber ground.
After disconnecting RF cables, don't forget to torque them using a dedicated torque wrench for SMA.
As of now, in-air cables on D6 are as follows.
D6 feedthrough number |
In-air Cable | Description |
F1 | ISC-307 | OMC DCPD |
F2 | ISC-409 | OMC PZT HV |
F3 | ISC-404 | OMC QPDs |
F4 | ISC-232 | OMCR DCPD |
F5 | ISC-233 | ASC-AS_C QPD |
F6 |
None |
Used to be OMCR pico, old ISC-235 cable was removed. No cable in chamber either. |
F7 | ISC-234 | AS_C pico |
F8 | ISC-317 | ASAIR Beam Diverter |
F9 | T-SAMS | OM2 heater |
F10 | ISC-236 | OM1 BOSEM |
F11 | ISC-237 | OM2 BOSEM |
F12 | ISC-238 | OM3 BOSEM |
AS_AIR beam position check
TJ and Tony installed viewport simulator on the +X door after adjusting the hoop positions on the real door.
From the picture I previously took (ASAIR_beampos.jpg), I know that the ASAIR beam position is about the radius of the BDV optic toward -Y direction at the BDV when it's open.
So I placed the camera so that the lens is co-axial with the line connecting the center of the ASAIR beam position by the BDV and the center of the ASAIR-AS_C splitter as good as I can (ASAIR_likely.jpg). Green cross is where I think the beam will be by BDV. Cyan line is the center line for ASAIR-AS_C BS. (Red line is the center line of the lens just so you know how big the parallax could be.)
Anyway, as far as the centering on the BS is not terrible, the beam will come out w/o any problem.
I also repositioned the camera to assess the worst case scenario (the beam will be very close to the left edge of the BS and therefore comes closest to the right edge of the viewport given the fixed position of the ASAIR beam by the BDV), and the beam will still come out of the viewport.
OMC TRANS beam check
We haven't done anything as there's no reason for a big change except that we changed how OMC ISC cables are routed inside OMCS, and that we removed OMCS suspension offsets. Just took one picture through the +Y hoop of the viewport simulator.
Table layout pictures
For posterity.
Couldn't take a good DCPD picture
I tried to take a good picture of at least one of the OMC DCPDs through the space between OMC shroud panels and through the OMC breadboard itself but I couldn't. The view is there but lighting is not (DCPD.jpg).
HAM7:
HAM6:
What's yet to be done.
Following up on Keita and Koji's converation, Sheila and I took a closer look at the OMCR DCPD in HAM6 to see if there are any cracks. We could not positively identify anything resembling a crack on the DCPD (images attached). We could also not see where the DCPD was hole punched. What is the typical size and placement for these holes? More images here. The DCPD is definitely quite dirty. We compared against some DCPDs of a similar design in HAM7 and can confirm that the OMCR DCPD is visibly much dirtier than those.
We also inspected the OMCR shroud input aperture for signs of pitting and other damage. There is no damage to report. We spent some time looking at the output aperture because we saw some potential damage along the aperture edge. After taking photos at various different angles to rule out reflections, we determined that apertures are fine, save for the occasional speckle on the shroud and the rouge edges likely left behind by the machining process. Images attached. More images here.
Today I took pictures and it really seems that the glass was cracked.
1st attachment is a cellphone picture, you can see something at the right edge. That thing never goes away regardless of your eye position and lighting.
2nd is a close up view from the side using a dedicated camera.
It seems to me that the front and the back surface of the glass each developed a scallop-shaped crack. I couldn't picture the hole in the can, not sure if this was actually punched or not, but I think the cracks are real.
You cannot see anything like this on the left edge of the PD (3rd attachment).
Sheila noticed that the two dots inside the PD can where the PD cables attach on this PD are vertically aligned. In the HAM7 SQZ PDs the dots are horizontal, e.g G:PD1, H:PD1, F:PD1. Is this fine?
Hi Camilla,
Not 100% certain that I know what you mean by "dots." I am assuming you are referring to the leads that penetrate the diode can. Either way, these are not quadrant photodiodes, so the rotational alignment of the photodetector element should not matter. It could be that you are comparing this device to other devices that use different models of photodiode, but again, the rotation of a single element diode will not matter.
Spare PD looks similar.
During installation I thought that we didn't have a spare OMCR DCPD, I somehow mis-remembered that everything we didn't use was sent to LLO but that wasn't true. So I took pictures of the spare too, and things look about the same.
1st picture was shot with a cellphone and an LED flashlight. It's not particularly difficult to take this kind of picture but note that the flashlight should be much brighter than the ambient light, and you should place flashlight as well as the camera such that reflection from the glass/metal/pd won't come into camera's view. You also avoid reflection of bright/white background coming into camera's view. You need to experiment.
2nd and 3rd picture shot with a stand-alone camera and a macro lens show some particulates are closer to the sensor plane (2nd picture) but more are on the glass plate (3rd picture). Cleaning the outer surface didn't change things so I assume these are mostly on the inside surface.
4th and 5th picture show the structure that looks similar to what we observed for the one in HAM6. Again this might be crack, but an alternative explanation that came to my mind is that a hole was successfully punched, which made protrusion of jagged metal edge of the hole into the can, and we're seeing that through a non-flat glass (it's apparent that the glass is not particularly flat around the edge, look at the last picture).
For inventory purpose:
PD-cable-enclosure assy |
Component: PD-cable |
Component: enclosure | Status |
D2100381-V2-S2200257 | D1600079-V3-SN1 | Spare | |
D2100381-V2-S2200258 | D1600079-V3-SN2 | WHAM6 |
(I'm 100% sure which component is in WHAM6. I couldn't find any record of which PD-cable-enclosure assy comprises which component, I just assume that younger components belong to younger assy.)
We calibrated OMCR DCPD using Pcal integrating sphere. Numbers are to follow. (But note that Koji is worried that maybe the cover glass for that PD was cracked when they punched a vent hole on the diode case.)
We fixed the beam dump that was too high.
After that, we investigated the DCPD signal ground (alog 65081) and we think we know the cause of the problem but we don't have an easy fix. We'll leave it as is.
It seems that one of the cables (either PZT or QPD) that goes to the OMC breadboard was touching the OMC shroud panel. We'll revisit that in the morning, adjust that, then confirm that the laser is still hitting the OMC QPDs. If not we'll realign.
It seems that we have ground loop problem (PZT shield is connected to the chamber). We'll revisit that at some time, maybe in the morning, or maybe after we're done with the injection from HAM7 to HAM6.
This is a belated followup of OMCR DCPD calibration. Following channels were calibrated.
Channel | meaning | Where | Caveat |
H1:OMC-REFL_A_LF_OUT_DQ | Power upstream of 99:1 splitter [mW] | Frontend |
gain=1, FM4/5/6/9 always ON. FM7/8 should be the inverse of H1:OMC-REFL_A_DC_GAINSETTING (e.g. enable "-20dB" if the gain is 20dB). If you set the whitening gain to anything other than 0dB, use FM10 to define an appropriate compensation gain. |
H1:OMC-REFL_A_DC_POWERMON | Power upstream of 99:1 splitter [mW] | Beckhoff | |
H1:OMC-REFL_A_DC_POWER | Power actually falling on the OMCR PD [mW] | Beckhoff |
I made the following changes for H1:OMC-REFL_A_LF filters, and coefficients were loaded to H1OMC.
Old | New | |
FM4 ("cts2V"), supposed to be 40/(2**16) |
gain(0.0006105) |
gain(0.00061035) (doesn't matter much) |
FM6 ("W/A"), supposed to be 1/responsivity. |
gain(6.5) | gain(17.15) |
FM9 ("inv(99:1)"), new filter, supposed to be the inverse of the transmissivity of 99:1 |
NA |
gain(104.17) |
Following is a table of parameters for Beckhoff:
old | new | |
H1:OMC-REFL_A_DC_OFFSET | -0.0025 | -0.0025 |
H1:OMC-REFL_A_DC_GAINSETTING | 20dB | 20dB |
H1:OMC-REFL_A_DC_RESPONSIVITY | 0.16 A/W | 0.058 A/W |
H1:OMC-REFL_A_DC_TRANSIMPEDANCE | 2000 Ohm | 2000 Ohm |
H1:OMC-REFL_A_DC_SPLITTERR | 100 % | 0.960 % |
Some details: