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
This morning I completed the weekly PSL FAMIS tasks.
HPO Pump Diode Operating Current Adjust (FAMIS 8453)
With the ISS OFF, I adjusted the operating current of the HPO DBs. The changes are summarized in the below table and a screenshot of the main PSL Beckhoff screen is attached for future reference.
Operating Current (A) | ||
Old | New | |
DB1 | 53.4 | 53.7 |
DB2 | 55.2 | 55.4 |
DB3 | 55.2 | 55.4 |
DB4 | 55.2 | 55.4 |
I did not adjust the operating temperatures of the HPO DBs. The HPO is now outputting 155.2 W and the ISS is back ON. This completes FAMIS 8453.
PSL Power Watchdog Reset (FAMIS 4024)
I reset both PSL power watchdogs at 18:54 UTC (10:54 PST). This completes FAMIS 4024.
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.
Calibration lines that are continuously injected in the interferometer are used to estimate time varying factors of calibration model which are in turn are used to correct h(t) in GDS pipeline. Since the calibration lines are of finite height, whenever there are strong glitches in the interferometer data the estimated time varying factors tend to be corrupted. To avoid these glitchy times, a threshold is used on the coherence based uncertainties at calibration line frequencies (using coherence between injected signal and DARM error). For C00 and C01, at LHO we used a maximum threshold of 0.4 %. The attached plot show the distribution of estimated uncertainties at various calibration lines during all of O2 (only observation intent times were used). We see that 0.4% is a little bit low, especially for PCal line 2 (331.9 Hz). From the plot, it seems any value above ~0.6%, outside the peaks of the distributions, will work fine. But we also don't want to go too large otherwise it would defeat the purpose avoiding glitchy times. At LLO we use a threshold of 2%. Since 2% satisfy our requirement of > 0.6% and also makes the thresholds between the two sites consistent, we could use 2% threshold for LHO also (for C02).
Was able to get ITMY tfs this morning. The stage 2 resonances are not super clean, but I'm think that's just because we are in air. Otherwise, looks okay.
The LVEA has been to transitioned to Laser HAZARD by Peter King.
Got the ClassA blanks installed and torqued down to 140" lbs. I can still see copper so they are not metal to metal yet. I was getting gun shy on the bolts and these will be replaced with the actual fiber feedthrus before a potential leak might be found or maybe even matters.
Trying to get close out tfs on BSC 2 and it appears the Corner 3 actuators are all swapped around. The H3 to H3 l4c/gs13 tfs for both stages look bad, but the H3 to V3 l4c/gs13 tfs look okay. I looked at the cables out of the coil drivers and the order of the labeling is the same for all 3 drivers, so I would guess that some work was done on the outside of the chamber and the cables weren't hooked back up correctly. First attached plot is the St2 tfs (with the cross-over tfs for corner 3), second shows the St2 corner 3 tfs, H3 to H3/V3 gs13s, V3 to H3/V3 tfs. The better looking tfs are H3 to V3 and V3 to H3, the crappy looking ones are H3 to H3 and V3 to V3. The St1 tfs are similarly confused, see third plot.
Checked the cables at the Chamber feedthrus--All are consistent Chassis/Cable Name: C2 F2 F1 C1 maps to label at feedthru: St1 V St2 V St2 H St1 H. Same for all three corners. The only thing at Corner3 is the strain relief zip tie is gone but that could have been for some time. I pulled each cable from the feedthru, noticed nothing to report and resecured.
Ed pulled the BSC2 corner 3 coil driver this morning and found that some cables inside were swapped left to right. He's fixed that and re-installed the coil drive. Corner3 tfs look good now. BSC2 is good to go.