Jeff K, Betsy, Rahul
Making a late entry for SRM rubbing investigation which happened last Thursday (see alog 79425). We went to HAM5 chamber and closely inspected SRM and all the EQ stops for any signs of rubbing. I couldn't see any of them touching/rubbing the chain, also at some places it was hard to see since the suspension is covered in shroud. However, at two places I felt the EQ stops were too close for my comfort, hence I very slightly adjusted them (to create a visible air gap) - first at optic barrel EQ stop and second at the metal upper mass stage.
Using a dental mirror I also checked the LF and RT bosem flags and found that that LF BOSEM flag is very close to the top LED/PD, with both offsets ON and OFF (was hard too spot any difference) - I am attaching a picture which I took on Jeff's phone. I did not adjust the LF bosem - since we didn't wanted to change the alignment.
Closes FAMIS#21186, last checked 76673
Cooling (attachment1)
Everything looking good!
Environment (attachment2)
Everything looking good!
Laser (attachment3)
Everything looking good
Stabilization (attachment4)
FSS_TPD_DC has drifted down to ~0.65, which is lower than it''s been in a while, and PMC REFL has continued to rise and is now sometimes surpassing 20.2
Mon Aug 05 08:05:25 2024 INFO: Fill completed in 5min 22secs
TITLE: 08/05 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Corrective Maintenance
OUTGOING OPERATOR: Tony
CURRENT ENVIRONMENT:
SEI_ENV state: MAINTENANCE
Wind: 5mph Gusts, 3mph 5min avg
Primary useism: 0.01 μm/s
Secondary useism: 0.06 μm/s
QUICK SUMMARY:
IFO is in MAINTENANCE for VENTING
This week we plan on closing remaining doors (HAM5) and prepping to pump down.
There was an emergency air instrumet issue Sunday Evening: alog 79443
Gerardo M., Janos Cs. After the aLog of Dave (https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=79442), we came onsite and found that the instrument air supply is not operational. In the reservoir tank the pressure was still ~80 psi, but the device 'as it is' was not operational; so the solenoid valve wasn't open to the system, and in general the whole system was off - which explains Dave's aLog 79442. When we arrived on site, GV6, GV7, and GV8 were already soft-closed. The following actions have been taken: - The instrument air supply was isolated from the instrument air system - A compressed air cylinder was hooked up to the system in the mechanical room (see picture), and we were slowly ramping up the air pressure, and so all the GVs opened up - GV7 was intentionally soft-closed after this, to prevent any undesirable X-manifold pressure raise, if GV7 decides to close - The X-manifold turbo was switched on, and after its pressure went below the pressure in the manifold, it was valved in. Now it is holding the X-manifoild's pressure at 3-4E-8 Torr. It will remain like this until the pumpdown (upside of the whole story that we will have the X-manifold turbo as an additional firepower during pumpdown) Other considerations: - As the instrument air system consumes the air very fast (from 1500 psi to 1000 in half an hour - note here that it opened all the GVs, so it won't be this bad all along), GV6 and GV8 can close before morning - To mitigate this potential issue, Nitrogen or compressed air cylinders will be hooked up to GV6 and GV8 directly, to minimize the losses (especially, if the air supply cannot be fixed quickly) - After the GVs soft closed in the beginning of this whole story, the pressures in the beamtube and in the CPs didn't change drastically, they followed the typical daily pressure cycles
Alarms have just been sent for low compressed air pressure in signal H0:VAC-MR_INSTAIR_PT199_PRESS_PSIG
24hour trend attached.
Sun Aug 04 08:03:48 2024 INFO: Fill completed in 3min 45secs
Short fill, but pressure spike looks good. Gerardo signed it off as a good fill.
Sat Aug 03 08:05:13 2024 INFO: Fill completed in 5min 10secs
TITLE: 08/02 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Corrective Maintenance
INCOMING OPERATOR: Nobody
SHIFT SUMMARY:
IFO is in MAINTENANCE for VENTING
HAM6 doors on as of 17:50 UTC.
Ryan C checked and turned on dust monitors - all except for known PSL102 are on. alog 79427.
LOG:
| Start Time | System | Name | Location | Lazer_Haz | Task | Time End |
|---|---|---|---|---|---|---|
| 14:31 | FAC | Karen | Optics, Vac Prep Labs | N | Technical Cleaning | 14:47 |
| 14:48 | FAC | Karen, Kim | LVEA | N | Technical Cleaning | 15:32 |
| 15:33 | VAC | Travis | LVEA | N | HAM5/6 Area Check | 15:46 |
| 16:00 | VAC | Gerardo | LVEA | N | HAM6 Doors Check | 17:48 |
| 16:02 | FAC | Tyler | LVEA | N | HAM6 Doors | 17:42 |
| 16:06 | FAC | Chris | LVEA | N | HAM6 Doors | 17:42 |
| 16:23 | FAC | Eric | LVEA | N | HAM6 Doors | 17:44 |
| 16:23 | VAC | Travis | LVEA | N | HAM6 Doors | 17:44 |
| 16:45 | FAC | Kim | H2 | N | Tech clean | 17:30 |
| 19:36 | OPS | Ryan | LVEA | N | Dust monitor check | 19:42 |
| 19:58 | PEM | Sam, Genevieve, Robert | LVEA | N | Missing BNC Reel | 20:49 |
| 22:08 | VAC | Gerardo | LVEA | N | RGA Check | 22:26 |
Closes FAMIS 26277
Laser Status:
NPRO output power is 1.821W (nominal ~2W)
AMP1 output power is 65.08W (nominal ~70W)
AMP2 output power is 137.6W (nominal 135-140W)
NPRO watchdog is GREEN
AMP1 watchdog is GREEN
AMP2 watchdog is GREEN
PDWD watchdog is GREEN
PMC:
It has been locked 24 days, 1 hr 50 minutes
Reflected power = 19.12W
Transmitted power = 107.6W
PowerSum = 126.8W
FSS:
It has been locked for 15 days 22 hr and 23 min
TPD[V] = 0.6675V
ISS:
The diffracted power is around 2.3%
Last saturation event was 16 days 23 hours and 36 minutes ago
Possible Issues:
PMC reflected power is high
FSS TPD is low
SEI seismometer mass check - Monthly - Closes FAMIS 26492
I've also attached the WD_ALL Mini Screen of what states the SEI platforms were in (FAMIS calls for DAMPED or ISOLATED but since we're venting, some of these are in different variants of damped or isolated.
Averaging Mass Centering channels for 10 [sec] ...
2024-08-02 13:21:31.272178
There are 27 T240 proof masses out of range ( > 0.3 [V] )!
ETMX T240 2 DOF X/U = -0.632 [V]
ETMX T240 2 DOF Y/V = -0.461 [V]
ETMX T240 2 DOF Z/W = -0.522 [V]
ITMX T240 1 DOF X/U = -1.764 [V]
ITMX T240 1 DOF Y/V = -0.302 [V]
ITMX T240 2 DOF X/U = -0.476 [V]
ITMX T240 2 DOF Y/V = -0.35 [V]
ITMX T240 2 DOF Z/W = -0.469 [V]
ITMX T240 3 DOF X/U = -1.844 [V]
ITMX T240 3 DOF Y/V = -0.387 [V]
ITMY T240 1 DOF Y/V = -0.472 [V]
ITMY T240 1 DOF Z/W = -0.611 [V]
ITMY T240 2 DOF Z/W = -0.629 [V]
ITMY T240 3 DOF X/U = -1.345 [V]
ITMY T240 3 DOF Y/V = -0.349 [V]
ITMY T240 3 DOF Z/W = -1.75 [V]
BS T240 1 DOF X/U = -0.594 [V]
BS T240 1 DOF Y/V = -0.928 [V]
BS T240 1 DOF Z/W = -0.457 [V]
BS T240 2 DOF X/U = -0.542 [V]
BS T240 2 DOF Y/V = -0.424 [V]
BS T240 2 DOF Z/W = -0.626 [V]
BS T240 3 DOF X/U = -0.712 [V]
BS T240 3 DOF Y/V = -0.676 [V]
BS T240 3 DOF Z/W = -1.191 [V]
HAM8 1 DOF Y/V = -0.505 [V]
HAM8 1 DOF Z/W = -0.812 [V]
All other proof masses are within range ( < 0.3 [V] ):
ETMX T240 1 DOF X/U = -0.133 [V]
ETMX T240 1 DOF Y/V = -0.112 [V]
ETMX T240 1 DOF Z/W = -0.159 [V]
ETMX T240 3 DOF X/U = -0.1 [V]
ETMX T240 3 DOF Y/V = -0.226 [V]
ETMX T240 3 DOF Z/W = -0.103 [V]
ETMY T240 1 DOF X/U = 0.022 [V]
ETMY T240 1 DOF Y/V = 0.09 [V]
ETMY T240 1 DOF Z/W = 0.148 [V]
ETMY T240 2 DOF X/U = -0.098 [V]
ETMY T240 2 DOF Y/V = 0.152 [V]
ETMY T240 2 DOF Z/W = 0.049 [V]
ETMY T240 3 DOF X/U = 0.155 [V]
ETMY T240 3 DOF Y/V = 0.041 [V]
ETMY T240 3 DOF Z/W = 0.089 [V]
ITMX T240 1 DOF Z/W = -0.092 [V]
ITMX T240 3 DOF Z/W = -0.289 [V]
ITMY T240 1 DOF X/U = -0.25 [V]
ITMY T240 2 DOF X/U = -0.08 [V]
ITMY T240 2 DOF Y/V = -0.185 [V]
HAM8 1 DOF X/U = -0.287 [V]
Assessment complete.
Averaging Mass Centering channels for 10 [sec] ...
2024-08-02 13:24:48.269297
There are 2 STS proof masses out of range ( > 2.0 [V] )!
STS EY DOF X/U = -3.98 [V]
STS EY DOF Z/W = 2.725 [V]
All other proof masses are within range ( < 2.0 [V] ):
STS A DOF X/U = -0.679 [V]
STS A DOF Y/V = -0.648 [V]
STS A DOF Z/W = -0.561 [V]
STS B DOF X/U = 0.287 [V]
STS B DOF Y/V = 0.996 [V]
STS B DOF Z/W = -0.446 [V]
STS C DOF X/U = -0.848 [V]
STS C DOF Y/V = 0.865 [V]
STS C DOF Z/W = 0.506 [V]
STS EX DOF X/U = -0.136 [V]
STS EX DOF Y/V = -0.016 [V]
STS EX DOF Z/W = 0.076 [V]
STS EY DOF Y/V = 0.037 [V]
STS FC DOF X/U = 0.24 [V]
STS FC DOF Y/V = -1.064 [V]
STS FC DOF Z/W = 0.627 [V]
Assessment complete.
Closes FAMIS#26320, last checked in 79324
Corner Station Fans (attachment1)
- Both MR_FAN2 accelerometers show the fan becoming noisier very erratically starting yesterday (08/01) at ~07:16UTC, so just after midnight Pacific time (attachment2). It looks like accelerometer 2 isn't getting as loud in the last 12 hours as it had been getting before that, but is still jumping around a lot. Accelerometer 1 however, looks like every time it jumps up, it's a bit louder than the previous time. Definitely should be checked out!
- MR_FAN6 1 starter getting a bit noisier 07/31 14:51UTC(attachment3), but it's a consistant noisy, and looking back at last week(attachment4), the noise levels had been similar last week before they were (I assume?) corrected.
- MR_FAN5 2, which had been pretty noisy last week, finally went down in amplitude five days ago
- All other fans are looking normal and within range.
Outbuilding Fans (attachment5)
- All fans are looking normal and within range.
(Chris S., Eric O., Travis S., Tyler G., Gerardo M.)
Both doors, ∓X, were installed on HAM6. No issues were encountered during the installation process.
TITLE: 08/02 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Corrective Maintenance
OUTGOING OPERATOR: Tony
CURRENT ENVIRONMENT:
SEI_ENV state: MAINTENANCE
Wind: 10mph Gusts, 6mph 5min avg
Primary useism: 0.03 μm/s
Secondary useism: 0.05 μm/s
QUICK SUMMARY:
IFO is in MAINTENANCE for VENT
Pardon the accidentally late alog (that never made it out of draft).
HAM6 Doors are back on as of 17:50 UTC.
As Ryan C reported yesterday, LVEA dust 5 is reporting a low battery and dust 6 stopped running 16:28 Wed 31jul2024 PDT. Attachment shows MEDMs and 7 day trends of 300nm particulate counts.
I power cycled DM6 which was frozen and I found DM5 unplugged so I plugged it back in and turn it back on. DM5 is in the cleanroom by HAM3 and it needs to be turned back off when we go back to observing(OPSInfo).
I was running the TFs for SRM to confirm that the suspension is good before we close HAM5, but the transfer function for L was a noticable amount lower in magnitude as compared to the measurements taken on July 17th right before we vented HAM5(pdf). We reran L but this time with the OPTICALIGN offsets turned ON, and the results matched our pre-vent measurements, which seemed strange and prompted looking into whether the RT OSEM has a problem. I've looked back at the state of SRM when the July 17th transfer functions were run, and T, V, R, P, and Y were run in DAMPED and OPTICALIGN offsets were OFF(T&R, V&Y, P). HOWEVER, when the L transfer function was run, SRM was ALIGNED and OPTICALIGN offsets were ON (P: 4254, Y: -9231)(L pre-vent). So that's why today's regular (offset OFF) L didn't match the pre-vent L, and why my second measurement of L with the offset on did match.
Yaw is the only other dof that was affected by the offsets being ON vs OFF, but the pre-vent Y measurements were taken with the offsets OFF, and these match with today's offset OFF measurements so we're all good there.
I'm not sure if there are still concerns about the RT OSEM on SRM M1, now that we know why L matches the pre-vent L, so I'm not sure if these results clear us for closing HAM5 or not.
Main set of measurement results (2024-08-01_2000) - SRM DAMPED, OPTICALIGN offset OFF:
$(sussvn)/HSTS/H1/SRM/SAGM1/Results/2024-08-01_2000_H1SUSSRM_M1_ALL_TFs.pdf
Second set of measurement results (2024-08-01_2200) - SRM DAMPED, OPTICALIGN offset ON:
$(sussvn)/HSTS/H1/SRM/SAGM1/Results/2024-08-01_2200_H1SUSSRM_M1_ALL_TFs.pdf
Full comparison of Pre-Vent, Post-Vent offset OFF (main) set, and Post-Vent offset ON set
$(sussvn)/HSTS/Common/Data/allhstss_2024_July17vAug01_H1SUSSRM_M1_PreVsPostOFIVent_ALL_TFs.pdf
I agree with Oli that SRM will be "as good as it has been between 2021 and 2024" if we leave it as is, but for different, more expanded reasons covered below.
To expand on Oli's "RT OSEM has a problem" -- the issue is that with the alignment offsets OFF, the RT (right) OSEM sensor / flag has expanded enough that the flag is only barely occulting the LED / PD beam, close to "open light." Thus the drop in magnitude response for Length and Yaw, the only two DOFs that use the RT OSEM. In fact, the M2 UL and M3 UL OSEMs, i.e. the lower stage left OSEMs are further *engaged*, close to "closed light." This is consistent with an overall positive yaw (+RZ) of the suspension w.r.t. the cage.
The *current* SRM alignment offsets are
(P: 1663, Y: -3095 [urad]) 2024-08-01, post OFI recovery and aux laser alignment, in air, HEPI locked
This digital request of *negative* ~3 millirads of yaw *centers* the OSEMs, implying that the OSEMs have been centered to the *alignment offsets ON* position. With the OSEMs centered, the magnitude of the response increases and looks cleaner because both LF and RT are contributing to measurement of the L and Y DOFs.
This checks out with the last time that we moved the OSEMs w.r.t. to the flags -- in 2021 -- see LHO:60576 where our goal was to keep the physical alignment of the optic the same, even though moving the OSEMs changes the digital request to get there. In that case, we kept the physical alignment and centered the top mass OSEMs to the alignment offsets ON, preserved physical alignment.
Importantly -- the result of the 2021 adventure of reproducing in-vac alignment while the IFO was in air was to leave the alignment offsets at
(P: 1738.28, Y: -3296 [urad]) 2021-11-08 (LHO:60578)
which is within 200 [urad] of the current slider values, and where the OSEMs are reasonably centered and responding well now.
These are also consistent with pre-vent in 2024 with OFI KTP damage in place, where with HAM5/6 HEPIs locked, a single-bounce IFO beam was used to find a good alignment
(P: 2192, Y: -3166 [urad]) 2024-07-17 (LHO:79246)
The offsets that Ibrahim used only on the L DOF during the July 17th health check, as Oli quotes, are:
(P: 4254, Y: -9231 [urad]) 2024-07-17 (LHO:79202)
which I believe were some very-lost, very-brief, temporary "I didn't realize HEPI was locked" alignment state used just prior to the official single bounce restoration later that day, LHO:79246, so the values of these should be ignored.
Finally, I attach a trend of the SRM alignment offsets over the last 4 months of sordid history with the OFI's KTP damage, covering both in-air and in-vac, HEPI unlocked and unlocked.
This also confirms that SRM's alignment, in all of these scenarios, is never needed to be outside of the
(P: 1600-2400 [urad], Y: 3000-3500 [urad])
range, i.e. less than 1 [mrad] from the 2021 positions (and the I suspect the large low pitch request after venting is the need to account for bouyancy of the optic, so really the alignment should stay within 0.5 pmrad] = 500 [urad] of those 2021 values.)
Note that this requested alignment range consumes a little less than half of the DAC range at ~50000 [ct] for the pitch OSEMs (T2 and T3) and yaw OSEMs (LF and RT).
Thus, if we just leave SRM alone, I suspect we'll be just as happy the SRM alignment and OSEM performance as we were between Nov 2021 until Jul 2024. This was the same decision we made in 2021. We'll just have to somehow remember that, for SRM, in order to get centered OSEMs to provide a OK performance on the top-mass "health check" transfer functions, we need the alignment offsets ON and in within 500 [urad] of (P: 2200, Y: -3300 [urad]). We can test where the boundaries of the alignment slider requests vs. RT OSEM performance decay during pump-down.
That being said, if we really want to mechanically relieve the yaw offset and restore centering of M1 RT (and M2 & M3 UL) we can...
Opened IIET Ticket 31769, to record that we've thought carefully about this decision to "let the 2021 OSEM position and SRM mechanical alignment ride," but that we reserve the right to try to mechanically offload *next* time. Hopefully the ticket and this aLOG series provides enough breadcrumbs to remember that we should relieve the alignment when we have the AUX laser set up already.
SUS HAM 5-6 System Wiring Diagrams D1002740
Grounding and Shielding at LIGO T1200131
Things to note:
1. HAM6 ISC cabling was not checked for ground loops
2. Short found on the OFI (cable SUS_SQ_30). Pin 13 shorting to ground. In-chamber ground NOT resolved.
3. All cables listed below passed testing:
SUS_HAM5_001 (SR3 Top)
SUS_HAM5_002 (SRM/SR3 Shared)
SUS_HAM5_019 (SR3 Middle)
SUS_HAM5_020 (SR3 Bottom)
SUS_HAM5_003 (SRM Top)
SUS_HAM5_025 (SRM Middle)
SUS_HAM5_026 (SRM Bottom)
SUS_ZM6_21 (ZM6)
SUS_HAM6_10 (OMC Top/Left)
SUS_HAM6_11 (OMC Right/Side)
ISC_236 (OM1)
ISC_237 (OM2)
ISC_238 (OM3)
In HAM5, Mitchell and I could not find the source of the shield grounding issue on the OFI AOSEM cable chain. We did the usual tricks:
1) Disconnected 25pin at the feedthru to see if the connector screws were touching the flange (no they didn't seem to be)
2) Made sre the 4th unused quadrapus cable end was not stowed anywhere that caused grounding to the shield
3) Fussed with/lifted/recoiled all of the coils in many places, no change to grounding.
In the past, when none of the above fix the issue, the entire cable length gets swapped out. However in consult with Kissel and commissioners, we did not feel these AOSEM control warranted needing to do this given that we are mid O4b. Opening a ticket to deal with this later.
J. Kissel, B. Weaver Picking up from the recommendations from LHO aLOG 60494 and LHO aLOG 60498 regarding what to do with the HXTSs H1 SUS SRM and H1 SUS SR3 OSEMs "issues" respectively, Betsy and I followed the recommendations for both SUS today, and centered all OSEM values such that they're at mid-range when the SUS are at the position they are when in-vacuum, during nominal low noise. For SR3, this was *very easy*, and just involved re-centering the M1 SD OSEM. Since SD is not involved in any alignment control, we merely need the flag position to sit in the middle of the calibrated range. So, Besty backed out the OSEM from its previous position at -76 [um], to ~0 [um]. For SRM, this was more of a process, but the process outlined in LHO:60494 actually worked really well. To the end user, though it may *appear* as though alignment of H1 SUS SRM has changed, if one solely looks at the DC position of OSEM sensors to reflect mechanical alignment, but this is not the case. Today's exercise proves (albeit crudely and imprecisely) that the actuation strength of the coil-magnet systems of the BOSEMs is roughly constant across/within the range the of the LED / PD shadow sensor system, and assuming such we successfully centered the OSEM sensors around the position of the flags when the coil magnet systems are steering the SUS into the place that the IFO is happy during nominal low-noise. I attach detailed notes of all the steps along the way, and I'll add a comment to this log that has the "in vacuum, during nominal low noise" trends that I used to inform where we want the SUS to be. The trends were taken from a ~24 hour stretch in May 2021, *after* we swapped ITMY and the IFO was aligned around a "point absorber free" ITMY. Note, because there is signficant low frequency DAC request from the global length and alignment loops when in nominal low noise, I recreated that additional requested DC position adjustment (beyond just the slider values) from global control by adding OFFSETs in Also of interest during this process was gathering the second ever open light current values for the M1 BOSEMs. As mentioned in LHO:60494, I dug up the first and only measurements from 2014 in LHO:60477, and we now have a definite measure of the decay of these 6 BOSEMS over 7.5 years. In short, there is ~20% decay in open light current. But, that doesn't mean I want to replace them -- my gut tells me "we still have time." Full data listed in the table below, with the new open light current (OLC) value in bold. OLC 2014 OLC 2014 OLC 2021 OLC 2021 2014-2021 2014-2021 (2014-2021)/2014 [ADC ct] [PD uA] [ADC ct] [PD uA] [ADC ct] [uA] [%] SRM M1 T1 26908 68.431 20585 52.35 6323 16.08 23.499 SRM M1 T2 25472 64.779 18996 48.309 6476 16.469 25.424 SRM M1 T3 28670 72.912 22119 56.252 6551 16.66 22.85 SRM M1 LF 27764 70.608 20831 52.976 6933 17.632 24.971 SRM M1 RT 26272 66.813 21110 53.686 5162 13.128 19.648 SRM M1 SD 25516 64.891 18715 47.595 6801 17.296 26.654 Note: even though we *measured* new open light current values, we did *not* update the compensating offset or gain. I'll need to think a bit more about that that means in terms of systematic error in the OSEM displacement calibration.
Here're a bunch of trends that I used to inform how much DAC / coil / magnet drive I should be putting on M1 in order to achieve an alignment of H1 SUS SRM that replicates the most recent good in-vacuum, nominal low noise alignment.
The time I used was around the time of May 09 2021 20:30 UTC.
Though the alignment swims around slowly on the ~12 hour timescale during the lock stretch, it's not that much, so I used the following DAC request to recreate the roughly equivalent alignment:
[urad] [DAC ct]
H1:SUS-SRM_M1_OPTICALIGN_P_OFFSET 1738.28 OUTPUT 3259.45
H1:SUS-SRM_M1_OPTICALIGN_Y_OFFSET -3296.41 OUTPUT -8836.36
[DAC ct]
H1:SUS-SRM_M1_LOCK_L_OUTPUT -5000
H1:SUS-SRM_M1_LOCK_P_OUTPUT 10
H1:SUS-SRM_M1_LOCK_Y_OUTPUT -120
H1:SUS-SRM_M1_COILOUTF_T1_INMON 0
H1:SUS-SRM_M1_COILOUTF_T2_INMON 54769
H1:SUS-SRM_M1_COILOUTF_T3_INMON -54769
H1:SUS-SRM_M1_COILOUTF_LF_INMON 53488
H1:SUS-SRM_M1_COILOUTF_RT_INMON -58488
H1:SUS-SRM_M1_COILOUTF_SD_INMON 0
(where, in case it's not clear, the LF RT OSEMs drive Longitudinal and Yaw, and the T2 T3 OSEMs drive Pitch.)
Just because I'm insatiably curious... ("were the OSEMs actually 'open lighted'?" so we're not confused between "actual LED decay" and just "a little bit of flag is still occluding the LED light") I also attach here a trend of the H1 SUS SRM M1 BOSEMs while Betsy has used the PEEK CAM nuts to have them longitudinally "backed off" from their flags.
It's ... too interesting if I look too closely (at the "10s of counts" level), so I'm going to ignore this, and justify it with the same argument I gave recently to a different SUS team in LHO aLOG 60179:
"you need not worry about a 50 / 30000 = 0.001 or 0.1% error in the calibration gain of 30000/OLC.
Conclusion -- 10s of counts error (or uncertainty due to environmental conditions) don't matter."
See that aLOG for full discussion.
Just prior to this recentering, I took a health check of the SUS in air with the ISI locked, using data from templates marked with the time stamp 2021-11-08_2000. Attached are the post-processed results. Nothing alarming here, just posting for comparison of data we *after* this change to the top mass OSEMS. (Well, not *change*, but re-centering as best we could around the in-observation alignment.)
Cross-referencing IIET Ticket 31769, which reminds us to revisit the mechanical alignment of SRM in 2025-2026, because in 2024, we decided to "let it ride," where "it" is the mechanical alignment kept, and OSEM positions we set, in this aLOG.