While the corner station old HEPI pump controller (aka the Ben Box) is down and before the new Beckhoff replacement is rolled out, I've created a dummy ioc which serves the old channels. This has "greened up" the EDC, it no longer has 31 disconnected channels. To appease the alarms system, the PRESSn channels have non-zero values which lie in the good range. CDS now has zero active alarms.
I took the opportunity to update my docs on testing/installing containerized IOCs.
TITLE: 05/19 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
SEI_ENV state: MAINTENANCE
Wind: 4mph Gusts, 1mph 3min avg
Primary useism: 0.02 μm/s
Secondary useism: 0.19 μm/s
QUICK SUMMARY: No alarms overnight, temperatures and dust counts looking normal. More alignment work in HAM2 planned for today along with continued prep on the BBSS in the LVEA west bay. CR workstations and wall FOMs are finishing their restarts.
Workstations were updated and rebooted. This was an OS packages update. Conda packages were not updated.
J. Freed
Update from last time 90231:
1. The funny set up from 90231 (IMG_0627.jpg) Was removed! *Clap*. The Spitter was moved lower on the rack and attached on the side of slot 11 with zip ties Photoon5-18-26.jpeg Photoon5-18-26at317 PM.jpeg. Note: The metal of the splitter was not separated from the metal of the rack, unsure if nessisary. Attinuators were added on each side of the splitter.
2. The 4096 Hz CDS DAC signal was tested and connected to the Double Mixer, the double mixer output was quickly checked on an osciloscope and nothing looked different from testing.
3. The current expected RF power going into the SPI prep chassis is 31.6dBm for both the meas and ref paths (Using 2x 10dB and 2x 2dB attinuators) which is slightly underpower of the expected 32 dBm. Screenshot2026-05-18at52906 PM.png I figure a slight underpower is better than an overpower. But will add a comment here if that changes. Will also check to be sure once the 2W amp is installed
4. Found a box of SPI cables that we bought, (whoops forgot about those). All cables in the current set up were replaced with the bought ones. All cables were also labeled.
SPI_HAM3_Linear_ish_Layout.png: I realized now the Screenshot2026-05-18at52906 PM.png picture is impossible to read clearly. I made a more "linear" and hopefully clearer picture of RF chain.
[Keita, Rahul, Elenna]
Today I moved IM2 and IM3 to bring the beam back to our reference position on IM4 trans QPD and center it on ISS QPD after Keita's move of the mode cleaner mirrors in 90259. This requires some iteration back and forth on both suspensions.
Our desired positon on IM4 trans is P = 0.22 and Y = -0.06. On ISS QPD, it is centered, so P=0 and Y=0.
We are driving MC2 in length, so the mode cleaner is flashing, and there are bright flashes on the QPDs. I am pausing ndscope on a flash and measuring the height of the peak in the fast channel and calculating the pit and yaw position from each QDP segment.
| Start | End | ||
| IM2 P slider | 765 | IM2 P slider | 810 |
| IM2 Y slider | -187.7 | IM2 Y slider | -88.7 |
| IM3 P slider | -560.7 | IM3 P slider | -614.7 |
| IM3 Y slider | 320 | IM3 Y slider | 385 |
| IM4 trans PIT | 0.390 | IM4 trans P | 0.268 |
| IM4 trans YAW | 0.450 | IM4 trans Y | 0.010 |
| ISS QPD PIT | -0.379 | ISS QPD PIT | -0.059 |
| ISS QPD YAW | -0.455 | ISS QPD YAW | 0.08 |
Unfortunately, this still results in clipping on the baffles Keita notes above, so we will keep going.
At the nominal IM4 trans position, yaw is pretty well centered. I then moved IM2 to both edges of IM4 trans QPD.
I changed the IM2 yaw slider to -250.7, which brought the yaw position on IM4 trans to 0.85. This made the clipping worse.
I changed the IM2 yaw slider to 90.3, which brought the yaw position on IM4 trans to -0.88. This was still not good enough to fix the clipping on the baffle.
By making a very large move to IM2 yaw slider value of 710.3, this centered the beam in the IM4 baffle. This is a ~800 urad move according to the osems and slider. The IFO REFL beam is still clipped.
I undid the 800 urad move, so the IM2 yaw slider is back to -88.7 for now.
Keita and Rahul went out to measure the position of the beam on MCs 1,2 and 3. We think that we need to make a move of these three mirrors to see if we can unclip the beam on these baffles that way.
We want to note that the positive yaw move of IM2 corresponds to unclipping on the IM4 baffle, this is consistent with the beam motion observed in chamber in the -X direction. However, this is contradictory to the sign on IM4 trans QPD, which was moving to negative yaw when we did this move. We suspect that the segment defintion must be wrong somewhere.
Keita will say more later once we have a chance to analyze the positions in chamber.
To clarify, the slider values of IM2 and IM3 are left at the "end" positions on the table above.
I trended the power measured at IM4 trans compared to the IMC input power for the entirety of the run. Some notes:
Because of this recalibration, I decided to compare both the IM4_TRANS_INMON and IM4_TRANS_OUT16 to IMC-PWR_IN_OUT16
FM10 in the IM4 trans filter bank is a factor that Craig and Georgia determined in the alog linked above, 4.606. I trended the inmon channel and multipled it by this number, ignoring other calibration factors present in the filter bank.
Therefore, the plotted ratio of IM4_trans [IN, OUT] / IMC power IN will help us understand how the power at IM4 trans changed throughout the run, like perhaps if the amount of clipping on the way to IM4 has changed.
I am comparing the ratios of both IM4 trans IN and OUT just in case we get confused by the changing calibration of the diode. I took an hourly median of these channels so we are not confused by random variation and masked the times to only show when IMC lock was either in state 100 (locked) or 70 (ISS ON).
Overall, the amount of power arriving on IM4 trans has definitely changed throughout the run.
Notably, during the vent between O4a and O4b, the amount of power measured at IM4 trans dropped. We chose not to move the IMs, and instead Sheila picoed to recenter on IM4 trans, linked above. Another power drop occured again during O4b. This time, we moved IMs to fix it. At the start of O4c is when Sheila and I recalibrated the diode, hence the disagreement with IN and OUT channels.
The second plot attached shows how the pitch and yaw on IM4 trans has varied alongside the power.
Based on what Keita can see happening in the chamber with baffle clipping, it is possible that during these alignment shifts, the amount of clipping in HAM2 on the IO baffles was changing, so the amount of power making it to IM4 trans and the amount of power going into the IFO was changing.
Specifically, I want to emphasize that with Craig's integrating sphere measurements in HAM1, we assumed that all loss between HAM1 and the PRM in HAM2 was known, i.e. loss from the IFI, etc. However, if there was additional loss on that path that changed with input alignment shifts, that would explain the apparent IM4 trans power changes during O4. Notably, Sheila and I recalibrated IM4 trans in O4c because after we fixed the input alignment in late O4b, we got more power on IM4 trans than we had gotten all run (see the jump around day 600 on the attached plots). I thought this was not physically possible, so we adjusted the calibration. Perhaps instead, we changed the amount of clipping in HAM2, giving us more light on the PRM than we had seen all of O4.
This may also help explain some of our arm power measurement mysteries if we actually had less input power than assumed.
I just want to add a clarification that we have been trying to replicate the alignment onto IM4 trans QPD, so we are trying to align to the previous pitch and yaw position. However, for O4, the beam was nearly falling off the ISS QPD, so we don't want to replicate that alignment (the pitch and yaw values on ISS QPD were like +- 0.9). We have decided to go with centering the beam on ISS QPD, especially since we have adjusted the ISS pico mirrors to find that alignment.
R. Crouch, B. Weaver, I. Abouelfettouh, J. Oberling, R. Thompson
Today we placed and aligned the BBS SUS cage on the WBSC2 ISI. In the morning we rough placed the SUS, and thought we had done a really good job on the first attempt. However, that was fed by a misread of how the Build/Inspect function in PolyWorks, well, works, and upon doing a more thorough measurement (directly measuring a constraining plane to inform SMR radius compensation instead of letting PolyWorks handle it automatically) we found there was a position and rotation error to the cage.
In the afternoon we moved the SUS cage around until things looked really good. We were well within our +/-1.0 mm XYZ tolerance, but once the SUS had been fully dog clamped to the ISI things shifted (as they do). In this case, it was roughly 0.5 mm in the +Y direction. All of our measurement points except one are within tolerance, so we called this good enough for SUS cage placement. To end, Ryan and I measured the circle that's defined by the lower section of the Figure 8 (the round section of the SUS cage that surrounds the BBS) on both the HR and AR sides of the cage. The first attachement shows the position deviations of the 4 points we used for cage placement/alignment and the current position of the HR and AR Figure 8; all except the Y axis position of 1 point are within our tolerance. The second attachment shows the rotation of the SUS cage w.r.t. the ISI; the angles listed are in degrees and are measured from the positive axes they are associated with (so X Ang is measured from the +X axis). These 2 lines show that the SUS cage is rotated roughly 400 - 500 µrad CCW (top-down view) from nominal.
Next up is to set up a total station looking at the AR face of the BBS to precisely align the optic to the ISI.
Ibrahim, Betsy, Randy, Jason, Ryan C
Today, we lifted the BBSS into the ISI. We then secured and aligned it with the help of IAS (Ryan C and Jason - seperate alog which will be linked later).
We used the aluma lift and dog clamps with the help of teflon pads to move the strucutre about the lift within dog clamp boundaries to align it to the ceiling to the model.
The alignment was done by touching the FARO SMR to the corners of the top of the lower structure to determine if translation or rotations were needed on the structure.
We also inspected BBS01 and found some particulate on the center of S1. Thankfully, it blew off using the N2 Top Gun.
Particle counts were checked in cleanroom periodically and were below 50 consistently.
See pictures.
TITLE: 05/18 Day Shift: 1430-2330 UTC (0730-1630 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY: Alignment work continued in HAM2 today, along with more prep of the BBSS and IAS surveying on the test stand. Since SPI alignment is ongoing on the optics lab, the laser remains on and running unattended with appropriate barriers and signage up.
LOG:
| Start Time | System | Name | Location | Lazer_Haz | Task | Time End |
|---|---|---|---|---|---|---|
| 19:43 | SAF | LASER HAZARD | LVEA | YES | LVEA IS LASER HAZARD | Ongoing |
| 14:50 | FAC | Kim | LVEA | - | Technical cleaning | 16:09 |
| 15:19 | VAC | Jordan | LVEA | - | Pump checks | 15:26 |
| 15:55 | FAC | Randy, Jeff | LVEA | - | Moving IOT2L a little | 16:16 |
| 15:55 | SPI | Jeff | Opt Lab | Local | SPI prep | 18:28 |
| 16:29 | IAS | Jason, Ryan C | LVEA | - | BS FARO surveying | 19:55 |
| 16:30 | ISC | Keita | LVEA | - | Opening lightpipe | 16:44 |
| 16:46 | SUS | Betsy, Ibrahim | LVEA | - | BBSS work | 18:34 |
| 16:52 | TCS | TJ | LVEA | - | Checking on TCSY water lines | 17:10 |
| 17:09 | SUS | Randy | LVEA | - | BBSS work | 20:09 |
| 17:18 | SPI | Josh | LVEA | - | SPI work at SUS-R2 | 18:32 |
| 18:04 | ISC | Keita | LVEA | Y | HAM2 beam alignment | 18:28 |
| 19:26 | SPI | Jeff | Opt Lab | Local | SPI alignment | 21:53 |
| 19:37 | ISC | Keita | LVEA | Y | HAM2 beam alignment | 19:47 |
| 20:10 | SEI | Fil | MER | n | HEPI electronics work | Ongoing |
| 20:10 | SPI | Josh | LVEA | - | SPI work at SUS-R2 | Ongoing |
| 20:11 | SUS | Betsy, Ibrahim | LVEA | - | BBSS work | Ongoing |
| 20:28 | SUS | Randy | LVEA | - | BBSS work | 21:38 |
| 21:06 | IAS | Jason, Ryan C | LVEA | - | BS FARO surveying | Ongoing |
| 22:24 | ISC | Keita | Opt Lab | - | Looking for parts | 23:02 |
| 22:44 | ISC | Rahul | Opt Lab | - | Looking for parts | 23:02 |
| 23:03 | ISC | Keita, Rahul | LVEA | Y | HAM2 beam alignment | Ongoing |
J. Kissel Picking up from last Friday (2026-05-15, LHO:90253), today I: - Secured D_R_P1 and D_M_P1 and confirmed that TFP REFL beams went into the dumps - Started aligning REF path and migrating optics over from the D2400107-v4 breadbord's CVM100 mounts into / onto D2400107-v5 IXM100 mounts: . R_M1 migrated. . Re-set up the power meter gantry assembly (since its only me, and I need the power meter stable for maximizing throughput thru irises) . Placed irises in holes 83 and 84, adjusted R_F1 and R_M1 to walk and align the beam thru irises, confirming with IR camera view of iris holes and power meter thru-put. . Secured R_F1 and R_M1 IXM mount 8-100 alignment screw shaft set screws, since these optics shall not move again. . R_B1 migrated. . Aligned beam through holes 86 and 95, repeating process above, but only adjusting R_B1. . Uncapped IFO_REF A and B PDs, PWRIN_REF PD and hooked them up to the o-scope (discovering a minor re-cabling issue; see LHO:90268) UNSOLVED SIDEQUEST (1) :: PWRIN_REF PD has a ~120 Hz oscillation on it. . R_B2 migrated. . Aligned beam through holes 98 and 99, repeating process above. UNSOLVED SIDEQUEST (2) :: Now, with D_FBR_PWRIN_REF so far away, the known issue with its PD seating within the generic enclosure means the PD reflected beam is ~2 inches above the board. Tried a huge 2"x3" dump but that was too big. . R_B3 migrated. . With nothing to align, just checked that beam went through irises in holes 100 and 97, and that beam looked well centered on PD. They did. . Migrated D_IFO_REF_B and D_IFO_REF_A, confirmed PD reflection landed on there and it did. Done for the day! The MEAS PATH alignment tomorrow!
Regarding UNSOLVED SIDEQUEST (2) :: Now, with D_FBR_PWRIN_REF further away [...] the PD reflected beam is ~2 inches above the board. Here're some picture to aide the discussion. I say "this is a known issue," because we'd encountered this particular PD's pitch of the diode when assembling the CVM100 version of the ISIK transceiver, D2400107-v4, but in that layout, the PD was angled away from the incoming beam in the opposite direction and the the dump was closer. We didn't have room behind R_B2 to have the same dump location with the upgrade to IXM100 mounts. None of the other PDs have this issue, the beam reflects back at the same 1 [inch] beam height that's the beam height for the board. We were in too much of a rush and had too little experience/expertise with these to consider cracking open the Generic PD enclosure (D1600083) to try to fix it. We suspect, in this Type 3 assembly for the FFD200 PDs, that either - the PD (line item 12 T1000573) is not seated well in its retaining ring (line item 4 D1600082), - there's a defect or something stuck between the retaining and its seat in the enclosure housing (line item 1 D1600079) - the retaining ring is not *exactly* the same size as the Q3000 for which it was designed and there's some slop in the assembly, or - the PD's pins were soldered into the PCB at an angle (line item 11 D1700116) But we're just guessing. This is S2401094, whose assembly technique is discussed in CIT:837 and record of completion is mentioned in CIT:898. Starting up the conversation with CIT.
Regarding UNSOLVED SIDEQUEST (1) :: PWRIN_REF PD has a ~120 Hz oscillation on it. See attached o-scope picture -- channel 3 (purple). 2V peak-to-peak wobbly 120 Hz oscillation on a 4.5 [V] mean. We've not tested this PD since we updated its transimpedance circuitry (see LHO:90105, and TIA Variant 3 D1002481 instantiation S2500713), so there may be a grounding issue there. Hard to believe it's the TIA op-amp itself, given that the RC feedback impedance we installed yields a 13.497 [kHz] pole. I've only tested the IFO MEAS and IFO REF channels of the Variant 2 chassis with light so far, but they don't show any issue. Laser power level on this PD during yesterday's test is the expected ~0.8 [mW]. I checked (but didn't re- or triple-check) that the electrical ground situation is well-managed. As in March 2026, the electrical ground of power supply feeding the TIAs banana'd-to-BNC'd-to-clip-doodled to the shield the o-scope's clip-doodle dongle whose signal is reading out PD ADC output voltage from a breakout board. Nowhere along this adpater/doodle/breakout/cable chain is metal touching metal. I'll look through the chain again, try reading it out differentially, and consult with local experts. It isn't a high priority right now, but we need to understand this before the transceiver leaves the optics lab.
FAMIS 63899
No major events of note; things looking very stable recently.
In preparation for testing out the BOSEMs on the BBSS, I've updated the OSEM2EUL and EUL2OSEM matrix values from the suspension projection values for the BSFM's geometry to projection values from the BBSS's geometry.
OSEM2EUL
before (BSFM projections), after (BBSS projections)
EUL2OSEM
Ibrahim, Betsy, Oli
Today, we installed BBS01 into the BBSS successfully.
BBS01 was on a table. BBSS was on the aluma lift. We picked BBS01 using the ERGO arm and slowly came into the optic. In this process, we:
On top of pictures below, 2 videos:
Wahoo! Congrats, y'all!
Note, current status as of last Thur was handoff to FARO IAS (Jason/Ryan C) who are up for mapping and guiding us into place. CAD files from CIT arrived Thur so quite literally just in time to get on it.
Also, thanks Travis for all the pictures.
J. Kissel SPI Wiring Diagram: D2400111-v6 In-chamber in-vac cable routing: In-vac Cable Routing Plan from G2401479-v3 I never aLOGged our choice of cable-table bracket floor assignment down when we originally assembled and signal-checked the D2400107-v4, so during disassembly in prep for upgrade to D2400107-v5 (LHO:90225) I took the time to write down the cable routing, cable serial number assignment, and cable table bracket (CBT) floor assignment: Path PD Name PD SN Duopus D9 CBT Name / Floor Quadrapus D25 CBT Name / Floor |----------D2600001--------| D1600083 Type 2 D2400341 D2000492 D2400343 D2000492 S2500512 IFO REF A/B S2401096/S2401095 S2500516 CBT 2 / 2nd of 2 cable E CBT 1 / 1st of 2 IFO MEAS A/B S2401097/S2401098 S2500514 CBT 2 / 1st of 2 cable D CBT 1 / 1st of 2 FBR PWR REF/MEAS S2401094/S2401093 S2500515 CBT 3 / 2nd of 2 cable C CBT 1 / 1st of 2 PD SN Monopus |----------D2600002--------| D1600083 Type 3 D2400340 OL ISIK QPD B S2401091 S2500518 CBT 3 / 1st of 2 cable B CBT 1 / 1st of 2 First and Second of the attached pictures are of the CBT 2 cable routing. I needed two pictures because the D9 end's two-part backshell of IFO REF cable was assembled with its serial number stamped on one side of one part, and the other side of the other part. C'est la vie. Third picture is of CBT 3's cable routing. The 2x D9 CBT assemblies (since the "type" we've assembled is not explicitly drawn in D2000492) are - QTY 1x D2000519 baseplate - QTY 1x D2000520 "Type 2" two-floor uprights, with - QTY 2x D2200443 D9 adapters, - QTY 2x 1/4"-20 x 0.625" L captive SHCS (95966A512) for securing to the HAM table (rather than the 3/8"-16 captive SHCS that are used to secure to the BSC tables) - QTY 2x #6-32 x 0.375"L SHCS (92200A146) for securing the baseplate to the upright - QTY 2x per D9 adapter (4x total) #4-40 x 0.224"L ("2D"; 1185-04EN224) nitronic 60 helicoils for each of the upright holes - QTY 2x per D9 adapter (4x total) #4-40 x 0.5"L captive SHCS (95966A140) for securing the adapters to the upright For the single D25 2-floor CBT that holds the D25 ends of the PD and picomotor quadrapuses, we used the standard D2000492 Type 2 configuration.
Pictures of the D1600083 Generic PD enclosure ends of the D2600001 Assemblies In order of their appearance in D2400111-v6 page 3: - IFO_REFA - IFO_REFB - IFO_MEASA - IFO_MEASB - FBRPWRIN_REF - FBRPWRIN_MEAS - QPD_B
The main aLOG's table of cables and the pictures of the cables are correct BUT my *labels* of the picture are wrong for the Cable Table Bracket #2 (also, I abbreviated Cable Table Bracket as CBT rather than CTB). I attach new versions of the pictures correctly labeled. Found this after re-achieving light the REF PDs today, as the IFO REF PD signals appeared on the SPI TIA Variant 2 ADC output CH3 and CH4 which should be the IFO MEAS PDs (per LHO:89775). Sure-enough, I had paired the IFO MEAS PD duopus S2500514 with the E leg of the S2500512 quadrapus, and the IFO REF duopus S2500516 with the D leg, because I'd followed the *labels* of the picture to reconstruct the cabling. All fixed now in the D2400107-v6 assembly (and I confirmed that the C and B legs are hooked up correctly to the FBR_PWRIN and QPDB correctly and match the table, pictures, labels and ADC CH assignment.).
We started with yesterday's alignment. I checked flashes in ISS array PDs and didn't like that the balances between them were very much different from how they were when IMC was locked back in March.
Then we started changing IM2 and IM3 to see if we can get back, but I was appalled that the flashes became stronger and stronger on array PDs as we aligned, which probably means that the beam was almost falling off of the PDs when we started.
That shouldn't have stopped us because we don't know where the beam was on the array PDs when MC was locked (people gave up optimizing that path because things didn't make sense), it could have been falling off of the diode (because each diode is 2mm, QPD is 3mm, the beam size is ~250um or so, and the beam was almost in one quadrant of the QPD). But I started thinking about many what-ifs and wasted time.
After all, since IM4 TRANS and ISS array QPD are both reasonably close to March 2026 position, we know that the beam position as well as angle of the beam injected into ISS path from IM4 are already close to those when IMC was good in vacuum.
What we should do is this:
Other things to note:
This is not required for the alignment but it's helpful to know how much we can move the beam on QPD. In an unlikely event where we somehow lose the beam in vacuum on the array QPD after IMC is locked, we might be able to scan IM3/IM2 to regain the beam on QPD, and slowly move IM3/IM2 back to the nominal position while pico-ing so the beam isn't lost on the QPD. If the beam is not clipped, the beam displacement on the QPD is ~3mm per 1mrad of IM3 rotation using parameters collected from various documents, see attached script.
The same script shows you that the Gouy phase separation between two pico mirrors is 10 degrees (if we use the beam parameter in Matt Heintze's alog 12537, which was probably obtained by the measurement of the bypassed beam) or about 20 degrees (if we use IMC eigenmode parameter propagated to the ISS path using D1200693).
Another thing is, if we believe the design eigenmode number rather than the measured bypassed beam in Matt's alog, the beam waist will be smaller and at about 20cm upstream of the PDs. The beam size on the PDs is about twice as large as it should be (470um rather than 250um). I cannot measure the beamsize of the flashes so we won't do anything, but that's something to remember. If IM3 has enough actuation range, we can later lock the IMC, scan the beam across the PD until the beam falls off, see how sharp the fall-off is, and use the diameter of the PD (3mm) to determine the size of the beam. Maybe a good project for a fellow.
One of the things that bothered me (that isn't directly related to ISS alignment) is the fact that we had to rotate JM3 by a huge amount, i.e. negative 200um in PIT to "center" the MC2 trans QPD. This is the equivalent of the negative YAW rotation of the beam in IMC's coordinates (clockwise seen from the top). Since the distance between MC2 and JM3 is ~19m according to E2400218, this means that the MC2 beam position was moved by about ~7.6mm in -Y direction on MC2. This seems to roughly corroborate with the pictures in alog 90203 ("before" picture and "after", hard to tell how much it actually moved due to parallax but there's no doubt that the motion was large).
What if this is because something is wrong with the MC2 trans path? Like the pico mirror in front of the QPD was bumped (by a huge amount, however unlikely it is). My conclusion is that we can lock IMC in vacuum, use WFS with MC2 centering, measure the centering on MC2 using dither, and figure it out. If QPD center is grossly off from the MC2 center, we can pico.
Sorry the script in the above alog didn't work because it was missing one line.
Attached is a working version. You need a la mode matlab package https://github.com/nicolassmith/alm.
J. Oberling, R. Crouch, J. Warner, B. Weaver, I. Abouelfettouh
This week we surveyed the position of the components that reside in WBSC2: The BS SUS cage (BSS), the ISI optics table (ISI Stage 2), and the 2 ITM Elliptical Baffles.
BS and the SUS Cage
The first picture shows our FARO survey of points on the BS SUS cage, chiefly along the bottom of the main support structure. These were surveyed by holding the FARO SMR against the hole being measured; the PolyWorks software handles the compensation from the center of the SMR to the point being measured. As can be seen, each point is very close in both X and Y axis position, being less than 0.1mm from its nominal location. The Z axis deviations are larger, but the largest of them is just over 0.25 mm, so every point is well within the positioning specifications used during installation and alignment in 2013.
Line 1 in the picture was created from the first and last survey points and represents the pointing of the BS SUS cage; all angles are reported in degrees. Some things to note here: I'm using the Acute Angle datum in PolyWorks, which is the angle measured from the closest axis. For the HR surface normal of the BS, the X Acute Angle is measured from the -X axis, the Y Acute Angle is measured from the +Y axis, and the Z Acute Angle is measured from the +Z axis. Since Line 1 is roughly perpendicular to the surface normal of the BS HR face, the axes the angles measure from are changed: The X Acute angle is now measured from the +X axis, the Y Acute Angle is still from the +Y axis, and the Z Acute Angle is now from the -Z axis. In addition, since Line 1 is nominally perpendicular to the BS HR surface normal I would expect the X and Y Acute angles to be swapped (BS X Acute = Line 1 Y Acute; BS Y Acute = Line 1 X Acute), but they aren't exactly. This appears to be a small error in the CAD model, if we make the assumption that the BS HR surface and the HR side of the BS SUS cage are nominally pointing in the same direction. This does, however, change the deviations for the X and Y Acute angles for Line 1. The table below shows what the data for Line 1 should be:
| Nominal | Measured | Deviation | |
| X Acute Angle | 44.9699 | 44.9073 | -0.0626 |
| Y Acute Angle | 45.0301 | 45.0927 | 0.0626 |
| Z Acute Angle | 90.0000 | 89.9661 | -0.0339 |
This means the BS SUS cage is yawed 0.0626°, or ~1.09 mrad, in the clockwise (CW) direction when looking from the top down (since Line 1 is closer to the +X axis than it should be). The Z Acute Angle represents a slight counterclockwise (CCW) roll of the SUS cage, when looking directly at the HR surface of the BS.
To attempt to better locate the BS in the IFO coordinate system, several measurements were taken with a ruler from points on the "Figure 8" section of the BS SUS cage to the BS optic itself. All measurments except one were done using a scale with 0.5 mm tic marks (so accurate to +/- 0.25 mm). The 10:00 "Figure 8 face to BS HR face" measurement had to be done using the side of the scale in inches, with 1/32" tic marks (so accurate to +/- 1/64") and then converted to mm (so accurate to +/- 0.4 mm). The measurements positions are listed like the BS HR surface is a clock, and assumes you are looking directly at the HR surface. The below table gives those results:
| Outside Edge of Figure 8 to BS optic edge (mm) | Front face of Figure 8 to BS HR face (mm) | |||||
| 3:00 (-X/-Y) | 6:00 (-Z) | 9:00 (+X/+Y) | 2:00 | 6:00 | 10:00 | |
| Measurement | 49.0 | 48.75 | 48.5 | 24.75 | 27.0 | 26.2 |
| CAD Nominal | 49.0 | 49.0 | 49.0 | 26.2 | 26.2 | 26.2 |
| Deviation | 0.0 | -0.25 | -0.5 | -1.45 | +0.8 | 0.0 |
The BS sits decently centered in the Figure 8 portion of the SUS cage, a little bit low and to the +X/+Y side. I would say not as much horizontally as it looks from the table, given the inherent error with reading the scale (the BS is not wider than its 370.0 mm specification, it's actually 0.15 mm narrower at 369.85 mm). The pointing implied by this measurement, however, is more than a little alarming. The 2:00 and 10:00 measurements show a significant yaw of the BS optic w.r.t. the SUS cage, and in the same direction as the yaw of the SUS cage as measured by the FARO. There is ~320.0 mm between the 2:00 and 10:00 positions on the BS, so that 1.45 mm difference in depth is a 4.53 mrad CW yaw. When added to the CW yaw of the SUS cage, this measurement shows that the BS optic is yawed 5.62 mrad CW from its nominal yaw. Even assuming the errors fall in our favor (so the 2:00 at 25.0 mm and the 10:00 at 25.8 mm), that's still a 3.59 mrad CW yaw (2.5 mrad BS and 1.09 mrad SUS cage). In addition, the 6:00 measurement implies a significant downward pitch of potentially several mrad, although with no way to measure the top of the optic we can't actually measure it. I have to be honest, I'm having a very hard time believing this measurement; we will revisit this once the BS cartridge has been moved to the test stand, where we have a better field of view for the FARO, more room to work and much better lighting around the BS, and can take direct measurements of the BS position and pointing using a total station and laser autocollimator (although there is no guarantee that the optic will be pointing in exactly the same direction after being craned across the LVEA). More to come on this.
ISI Optics Table
The second attachment shows the ISI positions as measured by the FARO. I've corrected the Z axis positions for the length of the rod we use to hang the SMR from the ISI so they give a better idea of the Z axis position. Not much can be said here, as LLO discovered that while these rods are good for measuring the Z axis position, they are not at all good at measuring X and Y. This makes sense as they were designed to be accurate in length and only length, so there's no guarantee that X and Y are repeatable. We plan on measuring the X and Y errors of this particular set of rods in the coming days (align to a table with a known hole pattern, attach the rod and measure with the FARO, repeat multiple times to see how the X and Y positions change). For now, we can say that the ISI is lower on the -X side vs the +X side, and lower on the +Y side vs the -Y side. I'm not alarmed by the deviations in Z axis position, as this ISI was supposed to be lower by ~2.5 mm (to place the BS in proper Z axis position, since it's lower in the IFO coordinate system but the SUS is the same length as the QUADs), but this was never captured in the CAD files.
ITM Elliptical Baffles
The final four attachments show our survey of both ITM elliptical baffles. Our view of the baffles and available fiducials to take measurements from were both limited, but we can say a few things.
ITMx Elliptical Baffle
We were able to get two points along the +Y bottom edge of the baffle, a single point along the +Y top edge, and single point near the center of the -X bottom edge of the baffle. From this I made a couple of planes that represent the +Y and bottom sides of the baffle and are shown in the third and fourth attachments; I, J, and K are the direction cosines of the surface normal of the plane, while the listed angles are the angle from the surface normal to the +X, +Y, and +Z axes. Interestingly, the point on the top edge looks very well aligned, within 1.0 mm all around, while the points along the bottom of the baffle are all low by several mm. In addition, there appears to be a significant upward pitch to the baffle. Jim did note that when attaching the transport bracket he had to push the baffle in the +X direction to clear ~0.5 mm at the point where the bracket attaches to the suspended portion of the baffle. This point is roughly 476 mm away from the baffle's suspension blade, so this is an ~1.05 mrad angle. Applying this same angle along the bottom of the baffle box gives an ~ -0.33 mm Z axis move of that bottom -X edge of the baffle, so this does not account for the measured deviation. In addition to the pitch, the bottom plane also shows a large roll (CCW when looking at the ITMx in WBSC3), while the side plane shows a large yaw (CCW when looking from the top down). We know these baffle panels aren't exactly straight, so it's hard to say if this significant pointing is also present on the elliptical hole of the baffle (we couldn't see it, so we couldn't measure it directly).
ITMy Elliptical Baffle
Similar to the ITMx baffle, we were only able to get a handful of points along the -X side and the bottom of the baffle. I made planes from these points representing the -X side and the bottom of the baffle (fifth and sixth attachments). As seen with the ITMx baffle, the points along the top of the baffle all look good while the points on the bottom are too low by several mm. There is a significant upward pitch to this baffle as well, as well as a large roll (CCW when looking at ITMy in WBSC1) and yaw (CCW when looking from the top down), although none are as large those as seen on the ITMx elliptical baffle. Again, we could not see the elliptical hole in the baffle to measure it, so we can't say if this pointing is an artifact of the panels or also present on the actual baffle portion of the baffle.
This completes our in-chamber measurements of the WBSC2 cartridge assembly, and closes LHO WP 13171.
I also want to note, Ryan and I also preformed some in-chamber FARO measurements in WHAM3 (ISI, MC2 SUS cage, PR2 SUS cage, MC2 and PR2 baffles) on April 10th; I will post those as soon as I get a chance to process the data in PolyWorks.
Some action photos while Jason & RyanC were chamberside at HAM3.
Ignore the very first table in the above alog, concerning the yaw of the BS SUS cage, as I apparently forgot how to do math when creating that. In writing a master alog trying to tie together the series of measurements we took on the BS (still a WIP) I went back to PolyWorks and, in a separate file so to not compromise the existing data, rotated the CAD model so the HR face of the BS SUS matched the target yaw of the BS HR surface. The results of that are shown in the attachment here. The angles listed for Line 3 are measured from the positive axis; i.e. X Ang is measured from the +X axis. Takeaways:
Honestly, ignore everything I wrote above about BS yaw. Not only was my math bad on the rotation correction (see previous comment), the error bar on the scale measurements used to calculate the yaw is so large that the only thing we can definitively say about the BS in-chamber yaw is that it is yawed CW w.r.t. the SUS cage.
As explained above, we did 2 measurements of the BS optic distance from the front face of the HR side Figure 8, one at roughly the 10 o'clock position and one at roughly the 2 o'clock position. The only Class B ruler we had at the time had mm on one side and inches on the other; the mm side had 0.5 mm tic marks for a +/- 0.25 mm error bar, while the inches side had 1/64" tic marks for an error bar of +/- 0.4 mm. 2 measurements were required at each position, one from the HR Figure 8 to the gold wire baffle and then one from wire baffle to the BS itself. Carrying the error bars from the multiple ruler measurements all the way through the yaw calculation yields a yaw of 4.53 +/- 4.06 mrad CW. With the error bar almost as large as the result, the only definitive thing we can say is that the BS optic was yawed w.r.t. the SUS cage, but we can't put an accurate number on it with the measurement method used.