- 9:02 am, Jason to CS VEA, HAM6 area, SR2 alignment setup.
- 9:05 am, Justin to X-End VEA, inspect ALS table.
- 9:05 am, Jodi to CS VEA, West bay area "to cause trouble".
- 9:09 am, Aaron to CS VEA, to pull cables for TCS cameras and fiber for hartmann sensor (Jodi said it and Aaron did it).
- 9:17 am, Thomas and David to CS VEA, assembly of periscope for Hartmann sensor.<-- done 10:45 am.
- 9:21 am, Corey to CS VEA, squeezer area to retrieve components.
- 9:23 am, alarm! alarm! BSC1, BSC2 and BSC3 SUS screens DOA, they were all frozen, we blamed Aaron and his pulling of cables, Jim B restarted all models.
- 9:50 am, Justin to X-End VEA, found something out of order on ALS table, tape on hand to fix it.
- 9:41 am, Betsy to CS VEA, inspection of HAM4 area.
- 10:12 am, Hugh to CS VEA, West bay area hunt for parts.
- 11:13 am, Jeff and Andres to CS VEA, work around HAM4 area.
- 11:42 am, David and Thomas CS VEA, TCS X-arm cabling and electronics.<-- done 12:08 pm.
- 1:18 pm, David and Thomas to CS VEA, more TCS work.
- 1:21 pm, Karen to Y-End VEA, to clean.
- 1:31 pm, Justin to CS VEA area transitioning to Laser HAZARD.
- 3:45 pm, David and Alastair to CS VEA, TCS Y-arm table inspection.
(Sheila, Alexa)
We had thought that maybe the 1/f noise seen in COMM came from the PFD. Today we have ruled that out. We did this by replacing the PFD with the spare IQ demod channels of the IMC. In this confirgaution we measured the beatnote signal to be 250mVpp, and set the COMM PLL Input gain to 31dB. This resulted in a loop with -18dB less gain than the nominal configuration. We then used the control signal to measure the noise.
I have attached a DTT with the following traces:
Clearly, the PFD does not seem to be the culprate. These measurements also suggest that we should lower the UGF of the COMM PLL loop.
With the demod in place and the input gain at 31dB, I also measured the amplitude spectrum out of the IMON of the demod. I have attached the data.
The VCO has a visible non-linear response, see second page here. If there is significant rms in the control signal at higher frequencies, this could potentially explain the excess noise.
Betsy, Jason
After rounding up step stools and tooling needed to be able to work in HAM4, I went into the chamber in order to mount the corner cube in front of the SR2 suspension for the first IAS sight shots. In order to set the corner cube mount into place I had to move:
1) 1" witness plate and assy that was vertically mounted on the front of the SR2 structure
2) 2 SR2 dog clamps of course
3) The large steering mirror (HWS?) parked in front of the sus structure and some of it's dog clamps.
As well, the witness plate that also in front of the sus structure will need to be moved as it is in the line of tool fire. I've removed the 1" witness optic and put it in a holder to ship back to CIT (presumably). We're still apparently sorting out what to do with the witness plate and optic which was placed by Kate on her last visit.
Other CC note: The particle counter in the SW corner of the cleanroom was consistently reading 14 or 25 for 0.3um particles, when I happened to look at it.
Jason will post X,Y,Z measurements of the optic position in HAM4. We've already started to tool up the SR2 sus to make the shifts he notes, but ran out of time to switch over to laser hazard. WIll resume tomorrow.
Here are the current X, Y, and Z position errors of the SR2.
I also want to note that we had to move a tip/tilt stage in the West side of HAM6 that was completely blocking line of sight to SR2. We will also have to move a tip/tilt stage on the East side of HAM6 as well as the OMC when we do the pitch/yaw alignment of SR2 in a couple days. Once we finish the longitudinal shift tomorrow morning I will begin re-setting my equipment for the pitch/yaw alignment.
Jeff B. brought to my attention that the purge-air flow in the combined volume of HAM4, HAM5 and HAM6 seems to be fluctuating in a periodic fashion -> I investigated and found that the low pressure output pressure regulator supplying purge air to the LVEA is stuck -> As such, the output pressure of the regulator (to the LVEA) is fluctuating between the nominal 1 psig and 1/2 psig as the input to the regulator fluctuates between the nominal band of 120 psig and 80 psig -> I'll order a part and get this fixed but in the meantime, in-chamber work can continue.
(Aidan B, David H, Thomas V, Matt H....Alastair H (remotely))
We have been trying to align the table the last few days, but ran into an issue with trying to get a good extinction of the beam reflected off the two "wavelength" branded polarisers that are after the Beckhoff controlled HWP.
First for a little bit of history. For the two table builds at LLO, the reflection off the 2nd of the polarisers after the Beckhoff controlled HWP could be minimised to a couple mW as measured by a power meter. (in fact I think I even heard could get down to 0.2mW). However, the two tables at LLO were built up only in "phase 1" build. Thus they do not have things like the AOM installed (which will be used for intensity stabilisation).
Here at LHO we are trying to do the phase 1 and phase 2 builds at the same time to work out as many issues as we can before trying to build up the other table at LHO, and do the phase 2 builds at LHO.
When doing the alignment the first time around, we found that for ~10W (about 20%) CO2 power we couldnt get the power reflected off the polariser to be anything less than ~10mW. We tried various times to fine tune the rotational angle of the polarisers as the power reflected is very sensitive to angle. However no success. We decided to simplify the setup to have a look at what was going on.
Firstly we put another HWP right after the ouput of the laser and then we looked at the performance of the very first polariser (II-VI brand) that is right after the laser. At an angle of 60 degrees on the HWP we got maximum transmission through this first polariser, and by fine tuning the angle of the polariser, we can get an extinction ratio of around 200:1 (p to s polarisation) which is what we roughly expected for the laser output (and double checked this was the case by removing the HWP and seeing that the results for what is transmitted and refected from the polariser essentially stays the same). So we are getting what we expect from the laser.
We then experimented with what we see when we placed wavelength type polariser after the AOM (so setup is laser, HWP, polariser, AOM, polariser). In this simple setup we couldnt get the reflection off the polariser after the AOM to be at a low power level like expected (we got around 0.43W at only 20% power level). Removing the AOM decreased the reflected power off the second polariser by around half this amount. We even tried moving the HWP to between the two polarisers and playing with it and looking at what we see, but minimum reflected power could get was still around 200mW (at 20% power setting of laser on PWM mode).
So decision was to make a real simple experiment and mimic what essentially LLO has (except for a bunch of steering mirrors between first polariser and Beckhoff controlled HWP). So we had a setup of laser, polariser, HWP (mimicking beckhoff controlled HWP), polairiser, polariser. With this setup we were able to get roughly the results see at LLO (ie a few mW of power reflected off the last of the polarisers when laser running in CW mode at full power).
So now went back and went for broke and put everything back as should before phase 2 layout (ie AOM back in, polarisers after beckhoff controlled HWP), and after realigning/checking alignment of everything, the minimum power we could get off the reflection of the 2nd of the polarisers after the Beckhoff controlled HWP when laser is in CW mode is ~95mW AAAAArrrrrggggghhhhhhh. At a hunch I ripped the AOM out (it only transmits the beam so should not affect the alignment pulling it out), and immediately the power reflected off the second of the polarisers after the HWP went down to a few mW.
Thus it seems the AOM is affecting the polarisation of the beam. We are going to look further into it (may be due to some kind of stress being induced to the AOM in someway), we may also look at changing the layout (move the first of the polarisers to after the AOM) to mimimise the affects of what the AOM is doing to the polarisation of the beam. The hunt goes on..................
All the BSC-ISIs foton files have been updated with the good switch output coniguration, according to the list posted in the SEI log (https://alog.ligo-la.caltech.edu/SEI/index.php?callRep=439)
I had to restart the h1guardian0 machine. Commissioners reported that the guardian IOC was still running, but the guardian processes were unresponsive and the log windows would not open. I was able to ssh into the machine, but could not run any command with the error "fork: no memory". Since I could not execute the "reboot" command, I rebooted the machine by pressing the front panel RESET button.
I am setting up sysadmin monitors on this machine to report processor space and memory usage. The machine had only been running for 7 days. Stefan reported that he was running a guardian in dry-run mode recently, other than that regular operation of guardian over the past week.
At about 16:42 UTC, I found the IRIG-B timing was off by more than 65000 on h1iopsusb123, and all user models had stopped running. Not sure what the cause was, a minute trend of the IRIG-B time showed it went bad about 16:23 UTC. I killed the user models (h1susitmx, h1susbs, h1susitmy), and restarted the h1iopsusb123 model. It came back in a normal state, so I restarted the user models. All is running OK at this time.
Jim reported some issues on ETMY HEPI yesterday https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=11618
Turns out that the position loops used were adding extra amplification at 10Hz (a 10Hz already amplified by the pier on this chamber). This was causing the HEPI to go unstable, dragging the ISI with it.
I switched to the controllers installed in FM2&FM3 (Cont_2), which are more generic, less aggressive loops. It works just fine.
ETMY chamber is used by the commissioners right now, but as soon as I have a chance I'll modified the design of the Cont_1 loops.
More info about this HEPI instability:
- This instability shows up mostly in Y (see ETMY_Sensors.png)
- This unstability is seen by the postion sensors and the actuators on HEPI (see ETMY_drive.png). The thing is that the HEPI-L4Cs, then the ISI-GS13s saturate (and make the platform trips) way before the IPS and ACT do.
- Find attached a screenshot of the actual filter installed. Removing the "bumps" at 10Hz and 45Hz fixed the problem.
2014_04_29 10:06 h1susbs
2014_04_29 10:07 h1susbs
2014_04_29 10:54 h1susitmx
2014_04_29 10:55 h1susitmx
2014_04_29 11:16 h1susitmy
2014_04_29 11:29 h1susetmx
2014_04_29 11:44 h1susetmy
2014_04_29 11:57 h1susetmx
2014_04_29 11:58 h1asc
2014_04_29 12:00 h1isiitmx
2014_04_29 12:10 h1susetmx
2014_04_29 12:12 h1asc
2014_04_29 12:12 h1susetmy
2014_04_29 12:22 h1isiitmx
2014_04_29 12:26 h1isiitmx
2014_04_29 12:29 h1sustmsx
2014_04_29 12:33 h1isiitmx
2014_04_29 12:34 h1sustmsy
2014_04_29 12:35 h1isiitmx
2014_04_29 12:49 h1isiitmx
2014_04_29 12:57 h1broadcast0
2014_04_29 12:57 h1dc0
2014_04_29 12:57 h1fw0
2014_04_29 12:57 h1fw1
2014_04_29 12:57 h1nds0
2014_04_29 12:57 h1nds1
2014_04_29 13:10 h1isiitmx
2014_04_29 13:25 h1isiitmy
2014_04_29 13:34 h1iscex
2014_04_29 13:36 h1iscey
2014_04_29 13:41 h1iscey
2014_04_29 13:41 h1isietmx
2014_04_29 13:47 h1isietmy
2014_04_29 13:55 h1isibs
2014_04_29 14:44 h1iscex
2014_04_29 14:45 h1iscey
2014_04_29 15:19 h1susomc
2014_04_29 16:03 h1susitmx
2014_04_29 16:07 h1susitmy
2014_04_29 16:11 h1iscex
2014_04_29 16:12 h1susetmx
2014_04_29 16:19 h1susetmy
2014_04_29 16:25 h1susbs
2014_04_29 16:32 h1suspr3
2014_04_29 16:42 h1susmc1
2014_04_29 16:43 h1susmc3
2014_04_29 16:45 h1susprm
2014_04_29 16:51 h1susmc2
2014_04_29 16:53 h1suspr2
2014_04_29 16:57 h1sussr2
2014_04_29 16:59 h1sussr3
2014_04_29 17:01 h1sussrm
2014_04_29 17:02 h1sussrm
2014_04_29 17:04 h1broadcast0
2014_04_29 17:04 h1dc0
2014_04_29 17:04 h1fw0
2014_04_29 17:04 h1fw1
2014_04_29 17:04 h1nds0
2014_04_29 17:04 h1nds1
2014_04_29 17:10 h1sussr2
2014_04_29 17:53 h1susetmy
No unexpected restarts. A very busy maintenance day.
Kiwamu, Arnaud, Sheila
We spent this evening trying to get UIM to test mass length to length measurements. We do this with no slow feedback to the top mass. With optical lever damping on, we saturate the PUM at high frequencies, so it has been easier to make the measurements with OpLev damping off. We have reasonable coherence from 5Hz down, saved as 2014-04-29_H1SUSETMX_L1_L2LPY_SwpetSine_OLDamp_Off_5Hz_to600mHz.xml
We are leaveing one measuremetn running on opsws6 with an envelope that we have tuned to get the low frequency part, saved as 2014-04-29_H1SUSETMX_L1_L2LPY_SwpetSine_OLDamp_Off_1Hz_down.xml.
We briefly tried using the UIM for feedback, with a theoretical plant inversion filter, with no obvious sucess.
Kiwamu fixed the calibration of REFL_Y_CTRL, makiing it identical to REFL_X_CTRL.
Sheila told me that a couple of OSEMs on the ETMY M0 stage were reading almost zero values. Since ETMY is a key for the upcoming DARM locking, I tried fixing them.
I went down to EY and spent some time trying to understand what is causing it. Finally I found out that this was due to a loose connection at a DB9 connector on a QUAD coil driver (D0902747). Since I was standing in front of the electronics rack with a flat top screw driver in hand, I tightened every DB9 connector which was in the same rack. This should increase a chance to detect gravitational waves.
Some detailed notes
JustinG, PeterK, RickS We went out to investigate issues with the PMC that might have caused it not to lock when the room temperature varied (Reported by Robert Schofield and others). The first thing we noticed was that the resonance threshold upper limit was set above the unlocked state level, which seems to indicate that the loop would consider itself locked even when it was not. We changed the upper level to 0.65 which was half of the unlocked level. I suspect that this was the cause of the problems with the automatic locking. We then adjusted the alignment into the PMC to minimize the reflected light level while the loop was locked. We reduced the reflected light monitor level from about 1.3 to about 1.0. However, we later noticed that the sum of the reflected and transmitted levels had dropped significantly. We re-visited the alignment and it seemed to be correct, with a calculated visibility (using the RFPD DC out, [unlocked -locked]/unlocked) of 92%. Something doesn't seem right with the PMC loop or the PMC itself. I suspect contamination windows and/or cavity. We measured the incident and transmitted light levels using the water-cooled power meter, 12 and 8 W respectively. Thus only 67% transmission with 92% visibility. We also looked at the FSS. We found that the beam was too high on the AOM and raised the AOM to significantly improve the diffraction efficiency. Then, we adjusted the retro-retlecting curved mirror to bring the beam up at the EOM position to achieve a single-pass efficiency (sqrt of the overall double-pass efficiency) of 86%. We then aligned into the Reference Cavity and measured a transmission efficiency of about 50%, consistent with earlier measurements. We then proceeded to measure the Open-loop transfer function of the Frequency Stabilization Servo but found that it was too low, about 150 kHz, even with the gain slider all the way up at 30 dB. The gain margin was only about 35 deg. This after increasing the power directed to the reference cavity and the reference cavity alignment. The phase of the FSS loop has a "bubble" centered around 400 kHz so the phase margin is about 25 deg. larger at 400 or 500 kHz than at 150 kHz. I'm somewhat surprised the performance was acceptable at all with what must have been a sub-100-kHz UGF. Don't have a simple idea for increasing the UGF. We need about 10 dB more gain. Increasing the light level incident on the PMC to 35 W, which we plan to do in June, will help. Otherwise, we will have to increase the modulation depth or increase the gain in one of the OpAmps on the FSS board. It appears that the Test2 input on the FSS is always enabled, even when disabled on the MEDM screen. Notes from today's work included below for future reference. Notes: April 29 2014 PeterK, Justin, Rick Mac mini OS 10.7.2 "medm_f" is the command to get fixed font sitemap PMC as found PowerRefl 1.3 W RFPD DC -0.138 V unlocked PowerRefl 11.3 W RFPD DC -1.25V 89% visibility resonance threshold 1.346 changed to 1.000 Tweaked alignment into PMC. Not much improvement 0.138 -> 0.130 Changed upper limit on resonance threshold from 1.0 to 0.65, half of the unlocked level FSS as-found locked state 0.028 mV at RFPD DC measured power after the AOM and iris 18.5 mW measured power after AOM and before iris 26 mW adjusted AOM height up and measured power now 23.35 mW after AOM and iris 27.35 mW total power of all beams double pass - started 14.3 mW...by adjusting beam upward return path increased to 20.35 mW double-pass efficiency = 74% single-pass (sort double-pass) = 86% measured power after EOM 19.9mW by dropping EOM .5mm meas pwr now 19.45 better centered on apertures Slow setting start point -0.2511 starting common gain 30.0 dB, fast gain 16.0 dB FSS RFPD dc level locked 19 mV FSS RFPD dc level unlocked 107 mV visibility 82% power incident on reference cavity ~14 mW power transmitted by reference cavity ~7 mw Measured power incident on PMC 12.3 - 12.5 W Measured power transmitted by PMC 8 W 1.289 reflected when PMC unlocked 0.099 reflected when PMC locked Note that the TEST2 enable does not appear to work for the FSS S/N S1107453, D040105
at 1082859581 could have been due to my kicking the suspension around
J. Kissel
We can't have a days worth of model changes, recompiles, reinstalls, restarts, and restores without at least one mystery. Today's casualty is H1SUSETMY's, M0, F1 F2 F3 SD cluster of OSEMs, which appear to be dead, reading out bit noise. I suspect this is an analog electronics failure that is merely coincident today's reboots, because the OSEMs that have failed are all on one satellite amplifer / coil driver chain. All other OSEM sensors appear fine. We'll have to check the analogue electronics in the morning.
The timeline of the day is as follows:
15:50:11 UTC / 08:50:11 PDT Event -- DC shift in OSEM values, with some ringing appears to be indicative of a ISI trip
18:42:35 UTC / 11:42:35 PDT Signals go dead -- corresponds with h1susetmy model restart at ~11:44 pm 00:02 PDT
19:56 UTC / 12:56 PDT Signals come back -- corresponds with h1dc0 framebuilder restart at 12:57 pm 00:02 PDT
20:47 UTC / 13:47 PDT h1susey model restart -- note the large temporal separation between the restart and the signal death.
~21:17 UTC / 14:17 PDT Signals die
23:19 UTC / 16:19 PDT h1susey model restart -- note the large temporal separation between the restart and the signal death.
00:04 UTC / 17:04 PDT h1cd0 frambuilder restart --- signals DO NOT come back
00:53 UTC / 17:53 PDT h1susey model restart, because I've noticed the problem, found the third bit of ADCO as red, assumed it was a too-speedy "make" and "make-install"
The last reboot did fix the ADC0 bit error, but it did not restore the OSEM values.
Note I'm retrieving the model restart times from the very useful model_start.log here:
/opt/rtcds/lho/h1/data/startlog/2014/04/29/2014_04_29_model_start.log
which is a daily log of all model restarts (a new folder and file is automatically created each day).
Mark B. and Gerardo
Yesterday (4/22/14) Gerardo and I measured the vertical mode Q of the OFIS for three different positions of the ECD block to try to get the Q in the specified range of 25-30.
The OFIS was set up on the optical bench in the H2 laser enclosure. The ECD block sits on a tray below the payload which is supported by four groups of vertically pointing screws at accessible positions around the edge of the structure. Gerardo had earlier attempted to set the ECD block at the nominal height using the spacer tool provided but found that this was too high and caused interference. He therefore lowered the block until it was just barely clear plus approximately an extra two turns of the 1/4-20 screws. This was our starting point for further adjustments.
To measure the vertical Q, we used the laser pointer and QPD from the monolithic violin mode setup and used a convenient screw on the top of the payload to partially block the beam. We displayed the "pitch" output of the QPD box on a digital oscilloscope with a 1 sec/div timebase and photographed the screen to capture the data. I read off the peak positions with GraphClick, and worked out the logarithmic decrement and Q with Mathematica.
For the initial position, the Q was 10.7. We lowered the ECD by one turn on all the screws and got Q = 18.9. We lowered the ECD another half turn and got Q = 23.3. Finally, today (4/23/14) we lowered the ECD another 3/4 turn and got 27.8, which is in spec.
Attached is a JPG of the setup, a PDF of all the screenshots, and for the fourth and final run, the Mathematica notebook, PDF thereof and the raw data.
We went back on Friday 4/25 and used the same method to measure the longitudinal (parallel to the OFI beam axis) and transverse mode Qs. For the longitudinal measurement we were able to keep the laser in almost the same position, just clipping a different edge, but for the transverse we had to send the beam on an odd diagonal path clipping one corner and then passing through the hole in the beam dump at the end (see photo). The results were
L: 21.3
T: 15.3
V: 27.8 (from 4/23, above)
The spec is <30 per T1000308-v1, p36, so these Qs look good and we propose to leave it like this.
I measured the gap between the copper plate and the magnets, 4 mm and all 4 corners.
Per request of Jeff Kissel, I extracted the frequencies from the data of 4/23 and 4/25 for the final configuration of the dampers: