Greg, Thomas
Darkhan and I moved the table back to HAM4 the other day, it's not quite in position yet because we haven't coupled to the viewport. After that, I set up an oplev laser to connected to the beam launcher so that we can align during laser safe.
Greg and I swapped M6, M7, M8, M9 , M10 and Source M2 silver mirrors for dielectric fused silica mirrors via ECR 1700295 for both ITMX and ITMY HWS. We aligned the mirrors to the current in-air beam path but since we've done some work in chamber and moved the tables around, we'll have to realign the in chamber beam path to the table before it's all said and done.
We still have to replace one more in-air beamsplitter with a mount that allows for larger aperture, but I'm still trying to locate it.
TITLE: 12/20 Day Shift: 16:00-00:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
Wind: 9mph Gusts, 6mph 5min avg
Primary useism: 0.03 μm/s
Secondary useism: 0.35 μm/s
QUICK SUMMARY:
Jeff B was covering for Corey and subsequently asked me to cover for him for a couple of hours this morning. Bubba and crew + Chris Soike are out putting doors on BSCs 1&3
While I was transitioning to laser safe this morning, I took the opportunity to turn off the clean room that was over HAM 4, and recently moved to accommodate the install of the NEG pumps. We should not need that clean room running for the remainder of this vent. I will continue to turn off clean rooms as we close up chambers and all are happy with results.
J. Kissel, T. Sadecki, B. Weaver
Betsy, Travis, and I have measured the standard top2top transfer functions for ITMX, BS, ITMY.
They are all clear of rubbing and we ready for doors on tomorrow. Wahoo!
Attached are processed transfer functions.
Note, for those who have doubts:
Some of the 1st (lowest frequency) fundamental modes appear a little bit squashed, but I'm confident that this is lack of coherence in the measurement: the BSC-ISIs are only damped with HEPI locked, it's a little windy out this evening (~20 mph), and the purge air is running full blast. A little difficult for the OSEMs to drive the whole suspension (i.e. the mode shapes for these lowest frequency modes) above that residual seismic noise. No reason to not put on doors, but we'll check again, as always.
Data files live here:
/ligo/svncommon/SusSVN/sus/trunk/QUAD/H1/ITMX/SAGM0/Data/
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_L_0p01to50Hz.xml
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_P_0p01to50Hz.xml
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_R_0p01to50Hz.xml
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_T_0p01to50Hz.xml
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_V_0p01to50Hz.xml
2017-12-19_2314_H1SUSITMX_M0_WhiteNoise_Y_0p01to50Hz.xml
/ligo/svncommon/SusSVN/sus/trunk/QUAD/H1/ITMX/SAGR0/Data
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_L_0p01to50Hz.xml
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_P_0p01to50Hz.xml
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_R_0p01to50Hz.xml
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_T_0p01to50Hz.xml
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_V_0p01to50Hz.xml
2017-12-19_2317_H1SUSITMX_R0_WhiteNoise_Y_0p01to50Hz.xml
/ligo/svncommon/SusSVN/sus/trunk/BSFM/H1/BS/SAGM1/Data
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_L_0p01to50Hz.xml
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_P_0p01to50Hz.xml
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_R_0p01to50Hz.xml
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_T_0p01to50Hz.xml
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_V_0p01to50Hz.xml
2017-12-18_1946_H1SUSBS_M1_WhiteNoise_Y_0p01to50Hz.xml
/ligo/svncommon/SusSVN/sus/trunk/QUAD/H1/ITMY/SAGM0/Data/
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_L_0p01to50Hz.xml
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_P_0p01to50Hz.xml
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_R_0p01to50Hz.xml
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_T_0p01to50Hz.xml
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_V_0p01to50Hz.xml
2017-12-20_0459_H1SUSITMY_M0_Mono_WhiteNoise_Y_0p01to50Hz.xml
/ligo/svncommon/SusSVN/sus/trunk/QUAD/H1/ITMY/SAGR0/Data
2017-12-20_0055_H1SUSITMY_R0_L_WhiteNoise_0p01to50Hz.xml
2017-12-20_0055_H1SUSITMY_R0_P_WhiteNoise_0p01to50Hz.xml
2017-12-20_0055_H1SUSITMY_R0_R_WhiteNoise_0p01to50Hz.xml
2017-12-20_0055_H1SUSITMY_R0_T_WhiteNoise_0p01to50Hz.xml
2017-12-20_0055_H1SUSITMY_R0_V_WhiteNoise_0p01to50Hz.xml
2017-12-20_0055_H1SUSITMY_R0_Y_WhiteNoise_0p01to50Hz.xml
Team left for the day after not getting very far in this alignment. Peter King worked on it this am, then handed to Jason and Sheila. Team is reconvening with the addition of Jenne and Rick tomorrow at 8am.
Today, Travis and I worked to closeout BSC 3 to finish out the set of chambers needing doors put on. We:
I attach a screenshot of the pitch transfer function during the Ring Heater cable rubbing. I also include illustrative drawings and pictures of the rubbing site. In words -- the ring heater cables (CBL7 and CBL 8 of D1001517), exiting the QUAD lower structure, should be sandwiched between the two inner face plates (aka "figure eights", D060462). On this ITM, it is not, and for the first time, it escaped far enough out of its designated path that it started to lightly interfere with the bottom of the main chain's UIM base plate (D060376). Attachments: First -- (from D0901346) A side view of the full solidworks assembly of the quad. The face plates are the long vertical blue things that extend the length of the lower structure. The two in the middle are the inner face plates. Second -- (from D1001838)An isolated view of the test-mass-side's inner face plate, with the fully assembled ring heater and cabling system. Third -- (from G1100850) Another view of the test-mass-side's inner face plate, with the fully assembled ring heater and cabling system. Fourth -- (from D0901346) A screenshot of the QUAD's solidworks eDrawing assembly, where I've hidden enough to show the ring heater cables, and made the face plates transparent. Naturally, the eDrawing is buggy, and the ring heater cables are displaced from where they're designed to be, and are actually interfering with the *reaction* chain's UIM base plate, but you get the point. Fifth -- a picture Betsy / Travis took of the offending cable rubbing against the *main* chain UIM base plate. Sixth -- (from D1001517) A screenshot of just the cable assembly to show what "CBL7" and "CBL8" are. Seventh -- A screenshot of the Pitch transfer function. Blue and Black are nominal, normal transfer functions. Red was while this rubbing was happening. As expected from the modes shapes of the middle-frequency pitch modes nominally at 1.33 Hz, 1.59 Hz, and 1.98 Hz, that had so clearly shifted, we knew that something was (wrong / rubbing) (in / around) the middle masses -- the PUM / UIM.
The second NEG pump of three was installed this morning on the H-1 output mode cleaner tube.
Ed, Sheila, Hugh
Today I removed the following from HAMS 2&3: ( all iris positions were photographed for convenient visual reference)
I got approval from Sheila and Hugh to leave the marker (xxxx640 type) for MC1 iris. It was the only other position that I could fit a clamp against.
The half-wave plate was still in-chamber when I left the area. It will come out as well. ISS work in that area of the table and too many bodies prohibited me removing it at this time. Sheila may have removed it. If not, then I will in the morning.
I was informed this morning that the 1/2 wave plate was, in fact, removed from the chamber.
I did pull the half wave plate out of the chamber. After talking with Betsy, we need to double about the dog clamps to make sure we are creating anything that interferes with SLC.
TITLE: 12/20 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
SHIFT SUMMARY: Still trying to close up, but getting closer.
LOG: (See attached)
After the ISC crew cleared the debris, and after scanning the table and wiping horizontal surfaces, removed one 1201 (50g) to give a slightly better float tilt. Lock/unlock shift is 8urad, -2urad, & 3urad for RX RY & RZ. Table left LOCKED.
Dan, Dave:
After sending all the system logs from raid-msr-e18-0-0 to Nexsan, Dan managed to clear the fault by performing a reset of controller-0. The system correctly failed over to the backup controller-1 and sent emails to sysadmin.
The vague controller-0 hardware fault occurred sometime on Saturday (12/16) and was reported in the daily status emails, but was not emailed at the time of the failure. This is a bug in the system since we have subscribed to all alerts.
Betsy called me out after they were done in BSC3, so I went out and unlocked the ISI, the shifts from the locked position are pretty good, considering the new optic. I've now taken tfs, they look okay with the typical caveats about in air measurements, with people working nearby. First attached plot shows the ST1 L4C tfs, second plot shows the ST2 GS13 tfs. ST2 resonances are a little fuzzy, ST1 resonances are pretty clean.
Sheila, Robert, Jenne
This morning Sheila and Robert confirmed that the IMs were aligned with the flashing IMC beam, and that the beam went through the irides near PRM and PR2.
We then determined that the DAC output of IM4 was unacceptably high (actually, we were railing it in order to get the beam aligned through the irides). Sheila loosened IM4's clamps and rotated it in yaw a bit, and tightened it back up. She then adjusted the pitch adjustment screw. After each adjustment we realigned the beam onto the PR2 iris to check the size of the DAC output. In the end, the largest DAC counts on IM4 are less than 50k, which is hopefully acceptable. IM2 has larger DAC counts (up to 71k), but we think that should be fine since IM2 isn't used for as much steering as IM4 is. IM1 and IM3 have smaller maximum DAC counts. I attach a screenshot so we remember what our in-air situation was, for next time we vent.
All three dust monitor vacuum pumps check out OK. Temps are good. Made slight adjustment to vacuum pressure at End-X. No other adjustments needed. End-Y is a bit noisy and there is carbon dust (from vanes) on the muffler. There is a standby pump staged at End-Y should this pump fail.
Whilst preparing to look at the beam headed towards the ISS photodetector array, we noticed that the
MC2 trans signal fluctuated whenever the Y-arm crane was activated (and/or was in motion).
The really spikey section of the attached plot is when the shutter was opened to admit light.
Jason/Peter
It seems that when the modifications were done to this particular chassis, there was an accidental swapping of wire harnesses when reassembling that was causing the team som difficulty. The swap I found was at the ISI Coil Driver Chassis Interface Board, connectors P6 and P9, which would swap the Coarse/Fine 1 & 2 Coil Driver Output signals. The unit was reinstalled and I'm waiting to hear the results of this correction.
Upon testing, Jim reported that the issue was resolved by this action.
[Maddie W., Aaron V., Greg M.]
Here is a summary of the filters and command line arguments that should be used for the C02 frame generation using the DCS calibration pipeline. This information is compiled from configurations wiki page and aLOGs linked from that wiki page. The command line arguments should be the same as for C01 except for changes noted in the table below. (Additionally, the frame names and channel names should be changed appropriately to C02.)
| GPS times | Filters files | Special command line arguments | Change from previous epoch |
|---|---|---|---|
1163173888 - 1167436818 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1163173888.npz |
--expected-fcc=347.2 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
N/A |
1167436818 - 1169326080 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1167436818.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Calibration model changes New H1 params file created on 1/3/2017 Coupled cavity pole frequency changed in reference model |
1169326080 - 1173225472 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1169326080.npz | same as above | New H1 params file created on 1/24/2017 (see aLOG 33585) |
1173225472 - end of run |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1173225472.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.004 --wings=(something larger than 600) --update-fcc --fcc-averaging-time=600 --fcc-filter-taper-length=32768 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Include EPICS to compute SRC detuning parameters NOTE: Starting with these frames there will be additional channels in the frames for the SRC detuning parameters |
After a discussion with the review team, we are just going to use a taper length of 32768 for both LHO and LLO. I have therefore just made this the default in the code. You do not need to set the --fcc-filter-taper-length option for C02 frame generation.
We have finished our rounds of testing and are settling on the options used to produce the X05 test frames (summary page here). Below is an updated table of the command lines to be used:
| GPS times | Filters files | Special command line arguments | Change from previous epoch |
|---|---|---|---|
1163173888 - 1167436818 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1163173888.npz |
--expected-fcc=347.2 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
n/a |
1167436818 - 1169326080 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1167436818.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --no-fs --no-srcQ --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Calibration model changes New H1 params file created on 1/3/2017 Coupled cavity pole frequency changed in reference model |
1169326080 - 1173225472 |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1169326080.npz | same as above | New H1 params file created on 1/24/2017 (see aLOG 33585) |
1173225472 - end of run |
aligocalibration/trunk/Runs/O2/GDSFilters/H1DCS_1173225472.npz |
--expected-fcc=360.0 --coherence-uncertainty-threshold=0.02 --wings=(something larger than 300) --update-fcc --fcc-averaging-time=60 --pcal-channel-name CAL-PCALY_TX_PD_OUT_DQ |
Include EPICS to compute SRC detuning parameters NOTE: Starting with these frames there will be additional channels in the frames for the SRC detuning parameters |