Another round of alignment, rubbing checks, TFs, rinse, repeat were done today. We got to the reaction chain positioned in approximately the right location with respect to the main chain in the longitudinal direction and the pitch close enough that the inter-chain bump stops are approximately equidistant. We decided to stop at this point to run some TFs, which, of course, showed some issues. We eventually got the main chain free of rubbing and took a full suite of low resolution TFs, enough to tell us that we are healthy and free-swinging.
For next Monday, we have on the docket to do some cable and ESD checkouts with EE and take a set of fully suspended violin mode measurements. Then on to fine alignment of both chains.
TITLE: 02/09 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
LOG:
15:52 (7:52) Bubba, guest to LVEA, Vertex
16:00 (8:00) Start of shift
16:16 (8:16) Hugh to LVEA
16:16 (8:16) Bubba, guest out of LVEA
16:23 (8:23) Hugh out of LVEA
17:15 (9:15) Peter to LVEA
17:19 (9:19) Peter out of LVEA
17:24 (9:24) Corey to Optics Lab -- Pick up parts
17:24 (9:24) Karen to Mid-Y
17:33 (9:33) Corey to LVEA -- Deliver parts
17:50 (9:50) Peter, Phil to End-Y, End-X -- Access control installation
18:05 (10:05) Karen leaving Mid-Y
18:06 (10:06) Corey back from LVEA
18:23 (10:23) Travis to End-Y
18:26 (10:26) Terry to SQZ Bay -- Place optics, label cables
18:26 (10:26) Sheila, Georgia to HAM6
18:37 (10:37) Richard, Phil, Peter to End-X
18:40 (10:40) Nutsinee to SQZ Bay
18:40 (10:40) Travis back from End-Y, going to Optics Lab
18:49 (10:49) Mark to Mid-Y
18:56 (10:56) Mark to CER -- Sticker delivery
19:00 (11:00) Mark back from CER
19:01 (11:01) Jason to LVEA -- Grab cart
19:12 (11:12) Jason out of LVEA
19:13 (11:13) Mark back from Mid-Y
19:14 (11:14) Richard back from End-X
19:50 (11:50) Jason to PSL enclosure -- Delivering equipment
19:57 (11:57) Jason back from PSL enclosure
20:10 (12:10) Evan to Electronics Bay -- Take photos
20:11 (12:11) Nutsinee out of SQZ Bay
20:15 (12:15) Evan back from Electronics Bay
20:42 (12:42) Corey back from Optics Lab
20:47 (12:47) Nutsinee to SQZ Bay
20:53 (12:53) Elizabeth to End-X -- Installing network switch
21:07 (13:07) Hugh to Optics Lab
21:10 (13:10) Betsy and Travis to End-Y -- ETMY work
21:19 (13:19) Elizabeth back from End-X
21:32 (13:32) Mark to Mid-X
21:52 (13:52) Nutsinee back from SQZ Bay
23:12 (15:12) Hugh to LVEA
23:35 (15:35) Ken back from Mid-X
23:49 (15:49) Travis and Betsy back from End-Y
23:59 (15:59) Hugh out of LVEA
00:00 (16:00) End of shift
Marc, Daniel
We installed the RF multipliers and the RF distribution amplifiers for the the 118.3 MHz (13th harmonics) and 72.8 MHz (8th harmonics) signal chains. The entire RF distribution chain now shows green. There is still a temporary 2W amplifier mounted at the bottom of ISC-C4 to drive the EOM.
[Georgia, Jenne]
With the new alignment after the arm peek and the locking of DRMI, we popped in to HAM6 to confirm that all of the clearances are okay, and the beam is well centered on all of the in-vac optics. Summary: we need a dog clamp (email already out to Corey to grab us some), and a teeny bit more work tomorrow, then we're done.
* Clearances seem good, although it would be good for another set of eyes to have a look at the shutter-closed wire clearance.
* We were a bit high on the last steering mirror and the lens in front of AS_C, so Georgia centered us up using the steering mirrors closer to the OM1 transmission point.
* We need to re-look at the AS WFS path. We're a little too close to the edge of the first mirror in transmission of OM3, but can't move the mirror appropriately until we have another dog clamp. Right now it's got one dog, and one bolt in a hole. But, we need to move another mm or so, and then won't be able to use the bolt hole. We're a little close in range on the steering mirror in front of AS_B, so we might also relieve some of that with the upstream mirrors while we're in chamber tomorrow. Also, the beam isn't centered well enough on the BS that splits the 2 WFS beams, or on the lens in front of that BS. So, basically the whole AS WFS path needs attention, but the first thing is that first mirror that needs a new dog clamp.
* There is a connection on the fast shutter that seems like it might be loose. Georgia will post a photo in a comment to this alog. We should make sure this is fully seated.
Here's the photo of the potentially dodgey shutter connection. I'm not sure what these are supposed to look, but it seems like it's on an angle and maybe not all the way in.
We went in today and successfully finished fixing up the AS WFS path.
There are 2 steering mirrors, a lens, and then the beamsplitter before the WFSs. We shifted the first steering mirror after OM3 position so the beam hits its center (clamped with a new dog), and steered this mirror to re-center the beam on the second steering mirror. We used the second steering mirror to center the beam on AS_A. We then re-centered the beam on AS_B with the mirror directly in front of it, this is now no longer at the edge of its range. The fine alignment was done using the AS-centering and OMC QPD loops.
TITLE: 02/08 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
16:00 (8:00) Start of shift
16:27 (8:27) Ken to Mid-Y
16:41 (8:41) Bartlett to cleaning area -- may open rolling door to receiving area
16:41 (8:41) Mark and Bubba to Mid-Y
17:27 (9:27) Bartlett back from cleaning area
17:42 (9:42) Mark and Bubba back from Mid-Y
17:42 (9:42) Mark to End-X, Mid-Y -- Grab clean room sock
17:56 (9:56) Kyle to LVEA, Mid-Y -- Inspect pipes
18:07 (10:07) Dave to CER -- Take photos
18:16 (10:16) Dave back from CER
18:50 (10:50) Hugh to End-X
19:03 (11:03) Nutsinee to SQZ Bay
19:07 (11:07) Phil and Richard to End-X -- Safety testing
19:29 (11:29) Hugh back from End-X
19:55 (11:55) Karen to Mid-Y -- Cleaning
19:59 (11:59) Phil and Richard back from End-X
20:12 (12:12) Jason and Robert to PSL enclosure -- Look for noise
20:15 (12:15) Nutsinee back from SQZ Bay
20:25 (12:25) Jason and Robert back from PSL enclosure
20:39 (12:39) Karen heading back from Mid-Y
21:12 (13:12) Bartlett to LVEA -- ITM camera work
21:36 (13:36) Phil and Peter to End-X -- Safety testing
21:37 (13:37) Mark to Mid-Y -- Put light bulbs in
21:42 (13:42) Hugh to Optics Lab, LVEA -- Look for cables
21:47 (13:47) Travis, Jim, Bubba to End-X
21:48 (13:48) Ed, Jason to Mid-X -- Grab amplifiers
21:56 (13:56) Jenne and Georgia to HAM6 -- Verify no clipping
21:56 (13:56) Bartlett out of the LVEA
22:23 (14:23) Travis, Jim, Bubba back from End-X
22:24 (14:24) Ed, Jason back from Mid-X
22:36 (14:36) Hugh out of LVEA
22:47 (14:47) Nutsinee to Optics Lab/SQZ Bay
23:41 (15:41) Jenne and Georgia back from HAM6
23:49 (15:49) Mark back from Mid-Y
00:00 (16:00) End of shift
-Commissioners going into HAM 6 late this week/early next week
-ITM cameras need to be locked down
-ITMY SAT amp swap next week
-ESD checkout set for Monday
-EX CR gross cleaning early next week
-EX move weld room (crane)
-HAM6 door off on Monday
-HVAC in lab ~Mar 5th
Tuesday Maintenance
-OAF Model
-ISI Model deferred ~Feb 20th
-DAQ Restart
Robert, Nutsinee
We have been having a mysterious SHG PZT drift at a rate of 2V/hr overnight when the table was shut and the fan was turned off. The downward drift kept on going for at least 20 hours without a sign of it turning back. The cause is still unclear (I will be posting more about this later in a separate alog). To gather more information we installed a temporary thermistor (a 200k Ohms resistor) near by the SHG housing to see how the temperature behaves around the area (the sensor will move around, for now that's where we started). The box is powered at 5V (external temporary power supply). We borrowed PEM patch panel for the input voltage and the read back. The read back is routed to the PEM rack by HAM4. The channel is PEM-CS_ADC_28_2k_OUT_DQ. The thermistor calibration is 100mV/C.
Terry, Daniel, Nutsinee
All four flippers now talk to Beckhoff and they work fine. The green pump flipper input was hooked up with a temporary cable for testing purpose, seed flipper doesn't have a read back cable hooked up yet (one of the two missing cables). Right now ON means flipper UP, and OFF means flipper DOWN. Nominal stage hasn't been set up for any of these flippers.
A quick guide to configure the Thorlabs MFF101 flippers with APT software:
0) Find a Window machine, download APT software from Thorlabs website (just look up the flipper model, software download is on the right). Run the .exe file and hit a bunch of nexts to finish the installation.
1) Hook up your flipper via a usb cable (should come with the flipper). Go to APT User found in Program file>Thorlabs. Not the APT Config that the software auto generates the icon on your desktop.
2) Confirms that your software and your flipper is talking to each other but clicking Position2 and Position1. Position2 is flipper UP, Position1 is flipper DOWN (in my case anyway, the manual says otherwise). This configuration is hard coded. Don't bother trying to change it. Once that's confirmed, go to Settings.
3) Digital I/O Pin 1 Operating Mode should be "Input: Goto Position" and the Digital I/O Pin 2 Operating Mode should be "Output: At Position". That configures your I/O input and output for Beckhoff communications. Check "Persist Settings to Hardware" box then hit OK. As far as I'm concerned. that's all you need.
4) Now try clicking Position1 button again. The flipper should flip and come right back up. That's normal. The flipper will only stay in down position as long as you hold the output value, you can't do that with the APT software, Beckhoff could.
And you're done.
Jenne, Georgia, Sheila
After yesterday's peak down the X arm, we worked on locking the vertex with our ITMX and input beam pointing set by the X arm.
We started with locking PRX+PRY, this worked fine, the refl spot is low and to the left on the REFL camera. We had to make some guardian adjustments throughout the day in places where we were using ASAIR sensors.
With PRX+PRY locked, we walked the RM alignments until they were close enough that we could turn on the REFL WFS centering loops.
We aligned MICH by moving ITMY, then later adjusted the beam splitter. We were able to lock MICH using the ASC_AS_B_RF45 sum, to do so we needed to flip the sign. We also reduced the gain setting by a factor of 2.
We locked PRMI without any problems, and adjusted the alignment by hand.
We then set the SR3 alignment for the new beam by feeding AS_C centering back to SR2 and moving SR3 until we started to loose power on AS_C_SUM. We set SR2 to center on AS_C, and searched for the SRM alignment that gave us SRY flashes. We were able to lock SRY using the new AS45 sensor, with a sign flip and no gain adjustment.
We locked DRMI, the only things that were different from the guardian default settings was that we reduced the MICH trigger from 20 to 7, and we have 3.3W into the IMC. We weren't able to turn on ASC but we will come back to that tomorrow.
With the new alignment, Sheila and I checked that we could resonate beam in the OMC. With DRMI locked, we turned the PSL injected power down until we had only a few mW in HAM6 (as measured by AS_C). Then we realigned OM3 and were able to turn on the regular OMC ASC loops (the centering loops for the AS WFS were already on). We ended up not getting the OMC to lock, but can certainly scan past resonances, so we should be fine alignment-wise with the OMC.
Ken (electrician) started to strip wiring from these two large gate valves as prep for upcoming CP4 Bake. Both GV11 and GV12 are hard-closed and locked out. The MEDM OPEN/CLOSE status is indicating YELLOW as the result of lifted limit switch wiring.
Dark gray button labeled SAF. System is still being commissioned.
Summary: Just after we opened up the chamber at EY, I got the chance to take photos of the P-Cal periscope from the point of view of the ETMY beam spot. The figures show that, in addition to glints associated with the camera mirrors, there were also glints from the periscope structure. A similar glint might explain why removing the mirrors at LLO did not completely get rid of the peaks in DARM produced by the periscope, and the glints from the structure motivate the work we are undertaking to baffle the structure. In addition to baffling the periscope structure, we may also need to baffle or angle the P-cal beam port.
The sources of the glints are finishing groves, which retro-reflect light where parts of their walls are normal to the direction to the beam spot. For linearly symmetric structures, this can happen only where the structures are tangential to circles around the specular reflection point, the place where a plane containing the line segment is normal to the path to the beam spot. I demonstrate glint control for such grooves by sanding samples in the radial direction, and suggest similar ways to control glints from other linear structures like corners, edges and folds. Such glint control might improve baffles or reduce the need for baffles in future upgrades.
Glints that retro-reflect scattered light are important because they can greatly increase scattering noise. Figure 1 shows the P-Cal periscope and indicates the various structures on the periscope. The expected glints from the two camera-periscope paths are visible and, in addition, there are a couple of glints from the support structure that are indicated. The two smaller images on the right side of the second page show that the major glint from the structure disappears when the camera and flash are moved only a few cm off-center of the test mass.
Figure 2 is a close up of one of the mirror regions on the periscope. An image of the second mirror of the ETM camera periscope is reflected in the closest mirror, and the reflection of the flash off of the camera port window and off of the flange around the window are also apparent. Periscopes are scattering dangers because they can image the test mass beam spot directly in front of and normal to the port, while the beam spot is at an angle to ports without periscopes.
In contrast with the camera periscopes, no similar glint is visible in the P-cal beam periscope mirrors. Unfortunately, the lack of glints does not completely alleviate the scattering concern for the P-cal beam periscope. The P-cal beam mirrors are narrow-band reflectors, unlike the broad-band camera mirrors, and there is a chain of 3 such mirrors before the camera flash reaches the port (note that the periscope structure can be seen through the mirrors). There has been a suggestion that the P-cal port flanges are producing scattering noise ( https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=39121 ) and I think we should baffle the flange and possibly angle the window unless it can be shown that the acceptance angle is small enough that it excludes the beam spot region of the test mass (the P-cal beams are, by design, offset above and below the beam spot on the test mass). It might be possible to check this by shining a laser in through the port and seeing if it can reach the location of the beam spot.
Figure 3 is a close up of one of the major glints seen on the first page. The concentric circles are drawn around the point on the periscope where the surface is normal to the direction to the test mass and so would reflect the flash right back to the camera located at the test mass. The glint can be seen to be in regions where the scratches or grooves are tangential to these circles. This is the case even in the upper right hand corner where irregular scratches are tangential and reflective. In the lower left hand corner of the image there is an abrupt change in groove direction and the glint ends abruptly.
The reason the glints only appear where the grooves are tangential to the circles around the point where the plane is normal, is that the walls of linearly symmetric grooves (linear symmetry in the sense that short translations along the line do not change the structure) can only tilt in directions perpendicular to the linear axis of the groove. So, surfaces of the groove can only retro-reflect at places where the linear axis of the groove is normal to the direction to the light source.
Figures 4 and 5 are images of the periscope taken when the camera was not at the ETM beam spot and show that the glints are again where the groves are tangential to the circles centered around the specular reflection point, where the plane of the surface is normal to the direction to the camera. The glints can change dramatically with only slight movements of the camera and flash as illustrated in the comparison of Figures 4 and 5. The reflection point has moved only a few cm from one side of a screw to the other.
Figure 6 shows the generality of this glint prediction, with the expected glints indicated by yellow arrows. Glints appear where the linear axis of linearly symmetric structures, such as folds, milling grooves, corners, bellows and edges, are tangential to circles around the point where a plane containing part of the linear axis would produce a specular reflection, where it is normal to the direction to the beam spot. Since many structures in the photo are in planes perpendicular to the main beam axis, this point is the same for all of the glints indicated by yellow arrows.
The corner reflection from the ACB, at the top right of Figure 1, is another example of a glint that occurs at the point where the linear axis (of the corner) is perpendicular to the direction to the beam spot.
The mechanism producing these glints suggests ways of controlling glints from baffles and in un-baffled structures. Figure 7 is a demonstration of glint control, comparing pieces that are milled or lathed to the same pieces after sanding so that the grooves could be oriented radially. This demonstration shows, for example, that if the down tube of the elliptical baffle were sanded along its long axis, it wouldn’t glint nearly as much.
Suggestions to help minimize glints for future upgrades:
The basic idea is to minimize surface regions which retro-reflect light to the beam spot because they are normal to the direction to the beam spot.
For linearly symmetric structures like edges, corners, or grooves, normal surfaces can be minimized by ensuring that the linear axis is never normal to the direction to the scattered light source, the optic.
An equivalent rule is to minimize regions that are tangential to circles around the specular reflection point of planes containing line segments of the linearly symmetric structure. This can be done by making the linear structures tend towards radial to the reflection point.
For the many structures that are in planes normal to the beam axis, the reflection point is on the beam axis, so this reduces to minimizing regions that are tangential to circles around the beam axis. Linear structures may be hierarchical, and the axes of linear substructures, like milling groves, also need to be considered. Where the structures must be tangential, glints can be minimized by overlaying radial grooves, as in Figure 7. Radial grooves (made by milling or sanding) in the glinting tangential regions of the frame of the elliptical baffle in Figure 6 would reduce or eliminate the glints.
Photographs like those in Figure 7, taken with the camera in the relative position of the beam spot, might be useful to fore-warn of glints from linear structures.
Robert S., Rick S.
TITLE: 02/07 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
LOG:
16:00 (8:00) Start of shift
16:00 (8:00) Ken to Mid-Y
16:21 (8:21) Peter back from PSL enclosure
16:27 (8:27) Christina to End-X, then Mid-X
16:40 (8:40) Phil to End-X -- HEPI pump controller work
17:21 (9:21) Kyle to Mid-Y
19:06 (11:06) Travis to Optics Lab
19:11 (11:11) Travis out of Optics Lab
19:13 (11:13) Karen to Mid-Y
19:14 (11:14) Travis to LVEA
19:24 (11:24) Travis out of LVEA
19:33 (11:33) Sheila and Georgia to ISCT1
19:50 (11:50) Sheila and Georgia back from ISCT1
19:54 (11:54) Karen leaving Mid-Y
20:44 (12:44) Peter, Phil to End-X -- Beckhoff work
20:54 (12:54) Betsy and Travis to End-Y
21:03 (13:03) Patrick to End-X solar panels -- Get model numbers
21:31 (13:31) Patrick back from End-X solar panels
21:51 (13:51) Ken back from at Mid-Y, going to End-X
22:15 (14:15) Terry to SQZ Bay
23:14 (15:14) Betsy and Travis back from End-Y
23:25 (15:25) Ken back from End-X
23:39 (15:39) Nutsinee to SQZ Bay
00:00 (16:00) End of shift
I noticed today that there is a large offset in V coming out of the ITMx M0 test bank. Trending this with Dataviewer, it appears to have started on the 19th of Jan. 2018. I perused the aLog for clues and asked the likely commissioning folk if they knew what this was about. I came up with no additional information (the ITMs were being used at the time for corner station commissioning, but no specific mention of a large offset in V on ITMx). Unless someone speaks up, this should probably be zeroed out before commissioning gets too far along.
This afternoon Travis and I worked on reattaching all of the main chain top BOSEMs which included adjusting the bracketry that holds all 12 main and reaction OSEMs. We started to look at TFs to make sure we are free enough to start pointing adjustments. However, after setting up TFs, determined there is still some slight rubbing, probably at the flags of the UIM. ANd so begins the iteration of alignment, rubbing mitigation, OSEM recentering, repeat.
To obtain TFs, did the usual settings change on the SUS:
BIO states of tops to 2.0 to 1.0
Turned off P and Y Test offsets, and took gains to 1.0
Cleared watchdogs on TMS and SEI in order to green all DACKILL watchdogs and allow EXC
In order to compensate for the missing mass of the new holey AERM optic being installed in the ETMY suspension, I had to rework the PenRe mass to be heavier. SYS had designed a heavier new set of parts to swap, and I'll report that the rebuild went smoothly - the weigh compensation was pretty spot on and the install of the parts which we have had fit troubles with in the past, went in easy (thanks to Eddie's tweak on the design based on my feedback).
For the record, the weights of these masses are as follows. Note, the idea is to make the old PenRe mass plus the old ERM mass weight equal the total of the new sets, such that the suspension hangs in the same vertical position as before.
OLD ETM01 mass | 25,993g | NEW AERM07 | 14,873g |
OLD PenRe mass | 53,236g | NEW PenRe mass | 64,356g |
Total | 79,229g | 79,229g |
Assembly weighs of the new PenRe:
OLD PenRe | New PenRe | |
Keeping Same Main Body | 29,857g | 29,857g |
Keeping Same batch of small parts | 3,002g | 3,002g |
Keeping Same wire clamp assys | 168g | 168g |
Cans and Plates (new and old species) | 19,087g | 30,284g |
Addable mass assys, to make total weight | 1,122g | 1,045g |
Total from above | 53,236g | 64,356g |
Doh - Typo, the ETMY AERM is AERM06, not 07.
The difference in weight between these 2 is a negligable 8g however.
Daniel, Sheila, Nutsinee
Nominal laser output power measured (with a PDA100A) as 18 mW through a 98% beam splitter (Rp 98%). Transimpedance=1500 Ohms, responsivity=.221A/W (variable gain setting on PDA100A set to 0dB).
Green output power measured (with a PDA100A) as 2 mW through 95% beam splitter (~100mW IR -> 40mW green). Transimpedance=1500 Ohms, responsivity=.313A/W (variable gain setting on PDA100A set to 0dB).
NewFocus 1611 detector to lock laser to PSL: Beat frequency signal measured with spectrum analyser ~ -14dBm at 155MHz as measured from the -1dB coupled output on the TTFSS pre-amp. Note there is a signal decrease by around 5dB with large (squeezing) laser frequency shifts (~500MHz or more) that seems to be due to beam pointing errors on the 1611 detector. However locking signal depends on phase and is largely insensitive to amplitude fluctuations so we should be ok. Responsivity=.75A/W, Transimpedance=-10k Ohm, gain setting 0, Voltage = -1.6V.
Power to 1611 detector: .30mW from PSL + .67mW from sqz laser -> .49mW on detector after 50/50 beam-splitter. MEDM screen reads .21mW ?? If the transimpedance is adjusted to -5k Ohm MEDM screen reads correct, but I suspect something is still odd about this.
Fibre (PSL) power rejected = 1.3 uW measured with a PD1A detector (2 K impedance).
Fibre (PSL) power launched = 27 uW measured with a PD1A detector from a 10% beam splitter. Disabled gain selection setting (alog 40161) has been corrected. Note the beamsplitter was changed from 2% transmission in the original drawing (BS8) to 10% transmission.
I calibrated three more PDs today. Both are Thorlabs SM1PD1A. Assuming a transimpedance of 2kOhms.
CLF Rejected PD: measured 4mW through a PBS cube. Responsivity = 4.1 A/W
Seed Launch PD: measured 9uW through a 98:2 BS. Responsivity = 4 A/W.
LO Launch PD: So little light gets through the 95:5 beam splitter so I measured the power before the beam splitter, take 5 percent of that and calibrate the PD accprdingly. The measured power (before BS10) was 85um. 5% of that is about 4um. I added 30dB gain to the detector and set the responsivity to 0.07 A/W to match what it's supposed to read.
The only photodiode left to calibrate is the CLF Launch PD.
CLF launch PD calibrated last week before the table was craned. Power transmitted was 44.4mW. Responsivity = 0.4 A/W.
Correction to the above comment, CLF Rejected and Seed Launch PD have resposivity of 0.41 and 0.4 A/W respectively.