I've completed the vacuum crate reboots as specified under WP4113. h0vemx, h0vemy, h0veey, and h0veex have all been rebooted using the new VxWorks boot server, vxboot, with no apparent issues (at this time). These are the last of the VME systems requiring reconfiguration, which means the old boot setup can now be retired. At the same time I moved these systems over to the new network switches installed in the outbuildings, in preparation for the old switches being removed.
PRM lower masses transfer functions from July 15th have been exported and are plotted in the attached documents below
(1) H1 PRM M2-M2 (July 2013) TF in 3 DOF (L P Y) plotted against hsts model (in blue) L1 PRM (July 2013 in orange ) and H1 PR2 (July 2013 in pink)
(2) H1 PRM M3-M3 (July 2013) TF in 3 DOF (L P Y) plotted against hsts model (in blue) L1 PRM (July 2013 in orange) and H1 PR2 (July 2013 in pink)
Both set of measurements are showing good agreement with the model, llo prm and lho pr2
Data, scripts and pdf files have been commited to the svn as of this entry
Note :
Since PRM M2 triple acquisition driver chassis hasn't been modified yet, the calibration factor in "calib_hsts.m" (living in sus/trunk/HSTS/Common/MatlabTools/) has been set to 0.32 mA/V, as described in the hsts electronics drawing summary. Value will need to be changed to 3 mA/V accordingly with driver's modif.
on opsws8, at 04-Sep-2013 09:35:28 PDT. It's gunna take 5* hours. *This is ridiculous! I can get this done in DTT in an hour. I'm gunna dive into the what-has-become 16 nested layers functions and find out why it's taking so darn long. Sheesh!
After "resting" one of the three cooling units in the MSR, here is the subsequent temperature increase (two day minute trend plot). The Temp probe is located on top of the racks at the mid point.
Attached are plots of dust counts requested from 4 PM September 2 to 4 PM September 3.
Transfer functions are running overnight on both HEPI-HAM2 and HEPI-HAM3.
In the attached spectra (stage 2 Z motion), the isolation is really good except at 6.18Hz. It seems that some electronic noise is reinjected in the system. Some noise hunt is ongoing.
V. Lhuillier, J. Kissel First, I had nothing to do with the performance of this spectra, but Vincent is far too humble. A factor of 20-50 below requirements between 0.5 and 1 [Hz]? A factor of 10 at 10 [Hz]? Totally spectacular. And this is *without* anything but position sensor control of HEPI, without GND to ST1 sensor correction, and by paying very little attention to degrees of freedom other that Y and Z. Spectacular work, monsieur. Second, this 6.18 [Hz] feature has been seen sporadically else where, as reported by the DetChar group at both sites (see, e.g. LHO aLOG 7159 and LLO aLOG 7976). Given the feature's characteristically, un-mechanical, sharp, Q, we are reasonably convinced the feature's source is either digital or analog electrical. The "best" guess -- and it's just one guess -- was that this is the beat note between two chamber's capacitive position sensor modulation frequencies (which are at a few [kHz]), where say, ITMY's ST1 H1 "coarse" sensor's master frequency (to which the remaining eleven are slaved) beats against BS's ST1 H1 sensor's master frequency, resulting in this sharp ~6-7 [Hz] feature. In order to test whether this is the case, we turned off*** all CPS in the entire corner station *except* for ITMY, and measured a quick spectra. The feature remained. So this is pretty solid evidence that it *is not* beating CPS modulation frequencies. The feature is *not* seen in ST1 sensors, and unfortunately the amplitude of the peak is just small enough to be hidden by residual seismic motion when the ISI is only under ST1 control, so checking if the feature is still present with ST2 OFF is tough. More ideas are welcome!! (Putting on my "does it really matter?" hat: unclear. Detchar as shown that the QUAD does a great job of filtering out this motion by the optic, as any good quadruple suspension would. Further, ~6 [Hz] is outside of the gravitational wave band. Given that it's a sharp feature, it really may not affect the performance of the IFO at all. It's just odd, and a glaring feature in the ISI performance plots that begs questions.) Finally, in the interest of improving the usability of the chamber seismic isolation (and for fun), I timed the world's expert in aLIGO BSC seismic isolation from a fully-cascaded chamber watchdog trip, to get back up to this level of isolation. I challenged him to it in under a half-hour ;-). In all seriousness though, I timed him. 5 minutes 31 seconds. And note, the clicking of buttons stopped around 4:30; the remainder of the time was spent waiting for things to settle down after the ramp up of the loops. This being said -- there were about 50 clicks to get there, and he was *flying* through them. So, assuming that we turn the 50 clicks into one click, and take the overhead associated with the clicking as the overhead that the one-button-click script would need to complete, I this ~5 minute recovery time is roughly what we should consider to be the irreducible. *** We turned off the CPS at the rack, using the separate ON/OFF rocker switch for the CPS in the back of the ISI Interface chassis -- which means the GS-13s and the chassis as a whole stayed powered *on* during this test. Note that "every ISI but the ITMY" includes HAM2, HAM3 (HAM4 and 5 are not yet running), HAM6, BS (ITMX is not yet running), and the ISI Test Stand.
Attached is a link the DetChar summary page with more info about these lines https://wiki.ligo.org/viewauth/DetChar/SUS7HzLineStudyPlots
- Fire Department briefly on site - Water refill - Mats changed - Concrete pouring for outreach - TMS at EX work ongoing - HAM ISI&HEPI testing - Initial alignment at test stand working on ITMX - HAM 2&3 commissioning measurements - Recovery from FW0 failure
Top mass was freed.
The cable buncle from the top mass to the ISI table was slightly bent and pulled so that it wouldn't lean on the edge of the top mass.
The top mass and the tele/table were both rebalanced.
BOSEMs were centered.
Temporary alignment stabilization toolings (D1100613) were installed and adjusted such that the ISC table barely sit on top of the set screws. We weren't able to find the new ones, and we weren't sure if new ones were made at all, so we used the old ones from H2 EY installation.Without these, mounting the alignment target by IAS will tip the TMS balance by a huge amount.
Now TMS is ready for IAS work, but unfortunately the large alignment target of IAS didn't fit the TMS tele, four screw holes should be made larger.
Dan repaired the SATABO/QFS disk system h1fw0/h1nds0 use. I restarted the framewriter at 12:27 today, prior to that fw0 would only run for about 10 minutes at a time so the frame file inventory is very disjointed.
Unit 1 in the MSR has been turned OFF. Units 2 and 3 are ON with setpoints 70F. Prior to this all three units have been running for several months since the repair of Unit 2.
Last Friday, I created a set of complementary filters with a 40mHz blend frequency. I computed newblend filters and installed them on stage 1. After turning on the isolation loops (level 3) and lowering the blend frequency at 40mHz on stage 1 and 100mHz on stage 2, I left the BSC-ISI (ITMY) isolated for the week-end. Note that the HEPI was controlled in position (100mHz) and the sensor correction was not engaged.
This configuration passed the 3-day week-end. I have attached a nice spectra of the stage 2 motion in the Y direction (seen by the GS13s).
GS-13 pod number 68 arrived with damaged flexures from shipping some time ago. After replacing the broken flexures, re-sealing the pod and filling it with Neon, I leak checked it in the modified VBO A. Initially I had some issues with an errant signal of Neon, but this was because I had forgotten to lower the ionizing voltage. Argon from a small air leak was doubly ionizing and appearing as Neon in the RGA. After lowering the voltage to 50v everything cleaned up nicely. The GS-13 tested good, coming out under the 3e-10 torr L/s leak rate requirement set by the VRB.
cdsfs1 went into read-only mode Friday evening between 18:20 and 19:20. At 17:45 this afternoon I rebooted the machine using the standard recovery procedure. Backups are proceding.
While looking at the system overviews I noticed that h1fw0 is not running. It has been unstable from about 16:45 this afternoon. Unfortunately fw1 is not perfectly stable, it had failed around 3pm and 5pm with short restarts. fw0 cannot run for more than a few minutes without crashing.
The console message on h1ldasgw0 shows many errors of type:
samfs: WARNING: SAM-QFS: ldas-h1-frames: cannot flush pages err=43 ....
I called Greg, he and Dan will investigate further. Sometimes fw0 gets to run for 10 minutes before crashing, so I'll keep both frame writers going to minimize the possibility of complete data loss. Greg will switch LDAS to using h1fw1 as the primary frame source.
Attached is a plot of the following 6 signals of that last 31h of IMC locking:
H1:PSL-FSS_FAST_MON_OUTPUT
H1:PSL-FSS_AUTOLOCK_STATE
H1:PSL-ISS_DIFFRACTION_AVG
H1:IMC-MC2_TRANS_SUM_OUTPUT
H1:PSL-FSS_TEMP_LOOP_OUTPUT
H1:PSL-PWR_NPRO_OUT_DQ
I didn't find a good PSL room temperature monitor, but I guess that all the fluctuations we see are temperature-induced in some form. See also elog 7593 for comparison.
- Corey, Andres, Hugh, Keita, Cheryl TMSX telescope moved by Genie from the TMS lab to the VEA. The telescope suspension wires were attached, and the telescope is now suspended. The upper mass is still locked by EQ stops. The vertical safety wire is installed, and the swing stop assembly is positioned under TMSX. A rod on the swing stop assembly goes through two eye bolts on TMSX, preventing it from swinging into the QUAD. Gymnastics of turning the telescope 180 degrees was documented more thoroughly in pictures today. The telescope safety support beams were installed Wednesday (my idea), which mean the Genie would not fit under the upper structure, so we rotated the front beam out of the way after removing 3 of 4 bolts. I returned to EX after lunch and attached the 4 cables to the ISC table. Cables come from the clamp in the center of the upper mass, attach to raised wire clamps, and connect to the cable brackets on the ISC table. They will need further tweaking after the upper mass is freed, to make sure they are not touching. Pictures added later.
Here are a few action photos from the TMS Table/Telescope install yesterday (& as usual, ALL TMS photo documentation is on ResourceSpace, here).
Pictures showing telescope optics protected by Alpha wipes, the swing top assembly, and cables. 1 - view from the floor - swing stop assembly on the left - telescope optics covered with large Alpha wipes 2 - swing stop assembly attached to TMSX 3 - CB-7 4 - CB-8 cables to upper mass 5 - CB-8 6 - CB-7 cables coming from upper mass 7 - CB-8 cables coming from upper mass For the cables in pictures 6 and 7, the peek zip ties are temporary to ensure connectors don't fall on the TMS optics.