J. Kissel
Took a set of Top to Top transfer functions for H1 SUS SRM this evening. Results look like the suspension remains free after Betsy & co re-engaged the OSEMs from having backed them off during the monolithic optic install.
Data lives here (and has been exported to files of similar name):
/ligo/svncommon/SusSVN/sus/trunk/HSTS/H1/SRM/SAGM1/Data/
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_L_0p01to50Hz.xml
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_P_0p01to50Hz.xml
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_R_0p01to50Hz.xml
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_T_0p01to50Hz.xml
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_V_0p01to50Hz.xml
2017-10-13_2122_H1SUSSRM_M1_WhiteNoise_Y_0p01to50Hz.xml
Will post detailed graphical results with the usual comparison against previous measurements and the model on Monday. Attached is a sneak peak of the Pitch to Pitch TF, the DOF usually most sensitive to shenanigans.
More detailed plots showing all DOFs. Confirms that the SUS is healthy and free thus far, after M2 & M3 OSEMs have been re-engaged to surround their magnets/flags. Never been closer!
The parts in question are D1101911 & D1101910.
HAM2: I've installed a QPD cable strain relief on IM4 trans. See first attachment.
HAM3: Done with MC2 trans and POPB, but not POPA.
For POPA, 1/4-20 screw wouldn't go in easily (I only tried for a minute or two) and I didn't bother to keep trying because I remember that this was a problem in the past for some of the QPDs (alog 19168 for TMSX).
One set of parts is left on the wire shelf on the work table in HAM2 cleanroom (top right of the wire shelf). If the 1/4-20 wouldn't cooperate, I would recommend to do the same solution as the above alog entry.
Done with ASC QPD strain rellief.
POPA strain relief was installed as planned using a long undersized screw (8-32), a nut, and some vent washers.
All segments of POPA, POPB, MC2 trans and IM4 trans responded to flashlight.
(Posted by Keita using Ed's account.)
F. Clara, J. Kissel, R. McCarthy, G. Moreno
After
- sorting out confusion with drive electronics (thanks Fil and Richard!)
- a few iterations of tuning transfer function amplitudes,
- realizing that the eddy current damping magnets may be interfering with / over damping the SUS,
- a tweak of a rubbing OSEM, and finally
- diagonalizing the longitudinal transfer function (i.e. actuating in Yaw to compensate for the SD OSEM's offset from the center of mass)
Gerardo and I have completed the first set of in-air, driven transfer functions with the recently installed OSEMs on the OFIS.
Attached are the results, and the resonant frequencies are as follows:
DOF Freq (Hz)
L 0.625 +/- 0.01
T 0.625 +/- 0.01
Y 1.039 +/- 0.01
This confirms that AOSEMs, driven with standard 16 bit, 20Vpp DAC, through a (LIGO) standard AI chassis, HAM-A coil driver and ISC/US-style satellite amplifier, pushing 3mm DIA x 6 mm LEN magnets is sufficient to drive the suspension. Further, the OSEM sensor has plenty enough signal to read out the position of the platform, so damping loops will be quite straight forward.
Excellent work design and assembly team!
Details
The data collection templates for the best, diagonalized transfer functions live in
/ligo/svncommon/SusSVN/sus/trunk/OFIS/H1/OFI/SAGM1/Data/
2017-10-13_2116_H1SUSOFI_M1_WhiteNoise_L_0p01to50Hz.xml
2017-10-13_2116_H1SUSOFI_M1_WhiteNoise_T_0p01to50Hz.xml
2017-10-13_2116_H1SUSOFI_M1_WhiteNoise_Y_0p01to50Hz.xml
Because the new SQZ electronics infrastructure is not yet in place, the drive chain is a temporary setup involving the digital drive chain of OM1 (hence the nonsensical denominator in the labels of the transfer functions), and several in-air cables, including a pin-flip ribbon cable (hence the poor coherence above 5 Hz).
Norna is suspicious of the OFIS's dynamical model put together by Mark Barton back in 2014, so hopefully this data can be used to solidify some degrees of freedom of the model.
I've created a new script that populates the new OFI's infrastructure with a diagonal sensor / actuator basis, which now lives in
/ligo/svncommon/SusSVN/sus/trunk/OFIS/Common/MatlabTools/
make_susofis_projections.m
where the conventions are defined as in E1700352, T1200015, and G1701887. Note I'm also sticking with the SUS convention to have the OSEM2EUL and EUL2OSEM matrices be the *transpose* of each other, and not the inverse. Taking into account that the LF and RT OSEMs (for driving T and Y) are equidistant from the suspended center of mass by l_LR_to_COM = 0.111 [m], but the SD OSEM is offset from the center of mass by l_SD_to_COM = 0.056 [mm], means the drive matrix is
| L | [ +r +r -1 ] | LF |
| T | = [ -0.5 -0.5 0 ] | RT |
| V | [ +0.5/l_LR -0.5/l_LR 0 ] | SD |
where r = l_LR_to_COM / l_SD_to_COM, and I've abbreviated l_LR_to_COM as l_LR. Actually sticking in the numbers, and reporting as they must be in the CDS system, that's
OSEM2EUL = +1.9821 +1.9821 -1.0000 EUL2OSEM = +1.9821 -0.5000 +9.0090
-0.5000 -0.5000 0.0000 +1.9821 -0.5000 -9.0090
+9.0090 -9.0090 0.0000 -1.0000 0.0000 0.0000
I have checked over Mark's OFI mode frequency results from his model linked from and reproduced in alog 12589 at https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=12589 They look fine to me. I have added a comment noting a typo in the list of frequencies in Jeff's comment to that alog. The numbers Mark used are fairly close to the current parameters.
TITLE: 10/13 Day Shift: 15:00-23:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:
LOG:
15:09 Garilynn into the LVEA
15:17 Betsy into biergarten
15:35 TJ out o HAM5 and then HAM2
15:39 Peter and Jeff heading ino PSL for water leak mitigation
17:04 Marc to MY
17:05 TJ out for a quick break
17:09 Gerardo into HAM5
17:36 Travis, Betsy, and Greg out of LVEA
18:12 TJ and Cheryl out to HAM2
18:15 Marc Back from MY
19:20 Gerardo ad Peter out to HAM5
19:21 Greg to biergarten to prepare chambers fo Monday work
19:27 TJ out for lunch
20:34 Gerardo and Peter back and Peter into the optics lab
20:49 Greg out and gone for the day
21:22 Arnab out to Y Cryopump area with Kyle
21:32 Richard out to CER
21:43 Peter and Gerardo out
Dust Monitor 102 has stopped responding in the last couple of hours and needs to be power cycled/re-started.
Failed dust monitors which need power cycling are usually accompanied with an invalid status on their HOLDTIMEMON PV (STAT = TIMEOUT). With this in mind, I've extended the code to mark channels which have zero std-dev counts with a preceding asterix if their holdmontime pv is also invalid. Example for PSL-102 which is currently bad:
H1:PEM-CS_DUST_PSL101 OK
*H1:PEM-CS_DUST_PSL102 WARNING: dust counts did not change, please investigate
H1:PEM-EX_DUST_VEA1 OK
Today the CDS overview screen looks like it has a bad case of measles (see attached). This is due to the h1ioplsc0 model ADC/TIM glitching now it has a faster computer. Like the end station SUS, some times the glitch propagates into the IPC channels and in turn glitches the receiver models. Because LSC touches more models than end station SUS, these glitches are more prominent.
Last night I added the LSC models to my script which issues diag reset to fast computer models and receivers of end-station SUS every minute. I'll extend it to cover receivers of LSC.
Jeff B, Dave:
I have re-written the check_dust_monitors_are_working script to make the output more readable.
The script defaults to checking the past 12 hours. Additionally it can take a second argument to check for N hours ending M hours ago, where N and M are the two arguments given. For each dust monitor, it internally checks both 0.5um and 0.3um dust counts. If both have shown no variation over the time period provided (i.e. both have zero standard deviation) then a warning message is printed, otherwise an ok message is printed.
Here is a "all is good" example for the past 12 hours:
check_dust_monitors_are_working
Checking dust monitors for possible problems over a period of 12 hours ending 0 hours ago...
H1:PEM-CS_DUST_LVEA2 OK
H1:PEM-CS_DUST_LVEA3 OK
H1:PEM-CS_DUST_LVEA4 OK
H1:PEM-CS_DUST_LVEA5 OK
H1:PEM-CS_DUST_LVEA6 OK
H1:PEM-CS_DUST_LVEA10 OK
H1:PEM-CS_DUST_LVEA30 OK
H1:PEM-CS_DUST_PSL101 OK
H1:PEM-CS_DUST_PSL102 OK
H1:PEM-EX_DUST_VEA1 OK
H1:PEM-EY_DUST_VEA1 OK
done
Here is an example with HAM6's monitor in error, prior to this morning's restart of the LEAV6‌ dust monitor:
check_dust_monitors_are_working 12 12
Checking dust monitors for possible problems over a period of 12 hours ending 12 hours ago...
H1:PEM-CS_DUST_LVEA2 OK
H1:PEM-CS_DUST_LVEA3 OK
H1:PEM-CS_DUST_LVEA4 OK
H1:PEM-CS_DUST_LVEA5 OK
H1:PEM-CS_DUST_LVEA6 WARNING: dust counts did not change, please investigate
H1:PEM-CS_DUST_LVEA10 OK
H1:PEM-CS_DUST_LVEA30 OK
H1:PEM-CS_DUST_PSL101 OK
H1:PEM-CS_DUST_PSL102 OK
H1:PEM-EX_DUST_VEA1 OK
H1:PEM-EY_DUST_VEA1 OK
done
Travis, Ed, Greg
We went down the x-arm to check if the cryopump baffle ring was grounded like the issue that Livingston had, alog 33667, where the ring was touching the copper pieces. One side was not centered very well, but was still clear of the copper block, the other side was pretty well centered. A quick bump test showed the baffle ring floating freely.
Images 667 & 669 (W side) show that there is no coupling between the copper of the baffle and the steel of the beam tube. It's pretty tight, but there is a gap. Images 670 & 671 are of the E side and there is a significant gap there. Your welcome for the "bump test". :P
Power cycled at 17:44. It's working properly again at this time.
Both doors on HAM 4 were removed this morning. HEPIs are covered also.
Everythin seems to be in working order this morning.
It seems that the data from the script output differed from the MEDM screen. Regarding HAM6: The terminal data showed 0.00 in both ranges despite the MEDM screen showing normal operation. CDS will look into this.
TITLE: 10/13 Day Shift: 15:00-23:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
OUTGOING OPERATOR: None
CURRENT ENVIRONMENT:
Wind: 5mph Gusts, 3mph 5min avg
Primary useism: 0.02 μm/s
Secondary useism: 0.19 μm/s
QUICK SUMMARY:
Kyle R., Rakesh K. Today we decoupled the 10" gate valve that isolates the YBM Main Turbo Pump (YBM MTP) from the Y-beam manifold. Next, we removed the 10" valve from the YBM pump port. For tonight, we are leaving the YBM 10" pump port covered in UHV AL Foil. Tomorrow we will install the valve and should make some progress towards re-coupling the the turbo to the valve.
With help from Mark and Tyler, Betsy and I reinstalled the ITMx lower structure into BSC3 this morning. In the afternoon, we worked on resuspending it to begin assessing alignment. Tomorrow, we will check the alignment at the OpLev viewport and begin adjustments.
TITLE: 10/12 Day Shift: 15:00-23:00 UTC (08:00-16:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:
LOG:
15:15 Vent meeting
15:57 Travis and Betsy ou to the biergarten
16:00 Jason and TJ out to LVEA
17:44 Jason out to HAM5
18:05 Travis and Betsy out
18:29 Jason and Garilynn out
18:40 TJ out for lunch
18:54 Bubba and crew taking the HAM4 South door off (started earlier, not sure when)
19:00 Dave B having Dolphin issues and the CDS overview is quite red with TCS Chiller imminent on Verbal Alarms and the PSL PMC not unlocked
19:05 Dave B out to EY to investigate Dolphin issue.
19:23 Dave back
20:00 Untripping IMs
20:02 Untripping MCs
20:03 Untripping PRs
20:05 Untripping BS
20:06 Untripping SRs20:12 Reset PSL EPICS alarm and readjusted ISS Diffracted Power
20:25 Marc to MY
20:39 Cheryl out to HAM2
20:44 Jason out to BSC1
20:57 Marc back
22:10 Betsy and Travis back out to biergarten
Krishna, Jim
This is a slight variation on an earlier duty cycle analysis by Jim. I'm trying to establish how the new ISI-Stage1 control scheme implemented in O2 at LHO benefited the interferometer. As a reminder, in O1, we only used feedback from the Stage 1 seismometer and switched between the 45/90 mHz blends to combat microseism/wind respectively. In O2 we used 'tilt-subtracted' feedforward at low-frequencies and 250 mHz blends as the nominal configuration on all platforms including the HAMs. The data lives in: SeiSVN/seismic/Common/Data/LHO_O1_O2_duty_cycle_data
The first attachment shows plots for duty cycle versus wind for O1/O2. It uses the minute trends of ISC Lock State and the ETMY windspeed (max) signal. The first page simply shows the distribution of wind - fraction of time windspeeds were in a given bin (bins were ~2 mph) during O1 and O2. The second page shows the fraction of the time the interferometer was locked at a given windspeed. Not only is there a clear improvement in O2, but the curve looks flat up to a windspeed of ~30 mph unlike in O1. The overall duty cycle in O2 seems to have suffered a bit, possibly due to other reasons. Pages 3 and 4 show similar plots, but only comparing the 45 mHz blends used in O1, which are still the default configuration at LLO. Again, it is interesting to note the downward trend on page 4 for the 45 mHz blend, which suggests that even 10-20 mph winds would begin to impact the interferometer.
The second attachment has very similar plots for duty cycle versus microseism velocity, using the band-limited-rms ITMY_Z (max) signal in the microseism band. The O2 configuration looks better once again and there is a similar trend of nearly flat duty cycle up to ~1300 nm/s velocities in O2. The distribution of the velocities looks odd/different, partly because of the inclusion of Hanford summers in O2, which are very quiet in the microseism.
I'm attaching the cumulative distributions of the wind and microseism (z) velocities (max of minute trends), so for example on the wind plot, the y-axis means that the wind is above ~15 mph about 15% of the time.
S. Dwyer, J. Kissel This completes the investigation of the broken beam dump found in HAM6 (see LHO aLOG 38918) -- the beam dump has been identified as the OMC REFL Beam Diverter Dump. This beam dump captures light *down stream* (toward the OMC) of the fast shutter. The dump was broken in a relatively clean vertical fracture which lines up with the dump's set screw, and when reconstructed appears to show a small pock-mark from an apparent small laser blast. While there's no way to prove why it broke, we have two main suspicions: - The black glass is secured to the dump's mount with metal set screws. It has been suggested that all such black glass should be secured with PEEK set screws. If not, these metal screws create un-due stress on the glass, especially if over-tightened. - During observation, it has become standard to leave the OMC REFL path's Beam Diverter CLOSED, i.e. blocking the path from hitting the OMC REFL QPDs and/or exiting HAM6 onto ISCT6. Thus, during some high-power lock loss in which both - the fast shutter protection failed, leaving the OM2 > OM3 > OMC > OMC REFL path exposed, and - the OMC was unlocked sending lots of OMC REFL light down the REFL path (instead of through the OMC, if it were locked). Picture highlights and labeled drawings are attached as .jpgs, and a more complete collection of pictures are compressed as a .pdf. Regarding the metal set screws on this dump: a survey of other similar beam dumps in the chamber indicate that *all* such dumps in HAM6 are secured with metal set screws (see 2017-10-11_HAM6_BumpDump_SetScrews.pdf). Open question: - Was the beam diverter closed when the shutter failed and killed the OMC DCPDs in Aug 2016 (LHO aLOGs 28820 and 28842)? - If closed, did we inspect this path / dump when we went in to fix the DCPDs? This picture from the Corey's Resource Space collection show that the dump is at least intact then.
Just in case, here's another labeled picture to show the beam path and clearance of the fast shutter to its high power beam dump. The above mentioned break is a result of the OMC REFL beam path, NOT the faster shutter path.
Now associated with FRS Ticket 9196.
Note, Corey and I both think (after looking at pictures) that these are the black PEEK set screws installed in the beam dumps shown.
Apologies -- in the above entry it says "when we killed the DCPDs in Aug 2016." However, we killed on of the OMC cavity mirrors, not the DCPDs (see, e.g. LHO aLOG 28820). We merely used the replacement of the entire OMC breadboard (necessary because the burned mirror is a part of the monolithic structure) as a target of opportunity to install high quantum efficiency PDs (see LHO aLOG 28807). Sorry about the confusion!