Joseph B, Darkhan,
Overview
Updated settings of CAL-CS oscillators and filters that are used for calculating calibration line coherences. These coherences will be used to inform the validity of the DARM time-dependent parameters calculated in the front-end.
At the moment the coherence outputs are 0, once we accumulate data at "low-noise" we should see cal. line coherence and uncertainty values.
The changes have been "accepted" in safe.snap and observe.snap
Details
The most recent version of CAL-CS update (see LHO alog 27733, LLO alog 26491) enabled calibration line coherences and uncertainties calculations in the front-end. These calculations require demodulation of excitation and DARM_ERR channels at line frequencies, band-pass and low-pass filters (see DCC T1600349).
Following Python script is used to set synchronized oscillators (in the "line coherence" blocks of CAL-CS) and the filters:
/userapps/trunk/cal/common/scripts/set_coherence_h1.py
An oscillator (for coherence calculation) that replicates an ESD line oscillator in SUSETMY model was set manually (see Attachment 1). Ideally this oscillator should give an equivalent output to the ESD line oscillator (currently SUS-ETMY_LKIN_P_OSC), but their amplitude ratio is ~10% different at the moment (see Attachment 2). Needs investigation.
Note that a possible source of an issue is that ETMY_LKIN_P_OSC is not a synchronized one. This might mean that every time this oscillator restarts the phase of the demod. osc. in CAL-CS should be adjusted for a meaningful κT calculation.
A screenshot of ESD line coh. demodulator and filters setup (as an example) is given in Attachments 3. Attachments 4-7 show CAL_CS_TDEP_*_LINE# MEDM screens.
J. Kissel As I'd seen charge continue to accumulate on the test masses (see LHO aLOG 28881), and we haven't been able to commission regular bias flipping since before ER9 (see LHO aLOGs 28362, 28152), I'd turned OFF the bias on the ETM ESDs last week Thursday (Aug 04) while we have HAM6 vented and the gate values are closed. After measuring charge today, this has had a noticeable effect on the accumulated charge, in that the majority of both test mass' quadrants show less accumulated charge. This may mean that leaving the bias OFF is just as effective at charge reduction as flipping the bias. I've left the BIAS OFF again after these measurements, to try to squeeze out as much more dissipation as I can. However, I still highly recommend commissioning the ability to flip the bias sign, once we have the IFO back and stable.
Krishna
I've attached some plots showing the tilt measurements with Compact-BRS. The calibration is only approximate right now (+/-50%). More accurate calibration will happen soon.
Quick Tutorial:
Recall that the instrument consists of a beam-balance with two fiber interferometer readouts at left and right ends of the balance. The fiber-tips are located on a translation stage driven by a PZT stack each (100V, 11 micron range). Photodiodes (PDs) measure the output of the interferometers. The PZTs are used in a low-frequency feedback loop to keep the PDs at mid-fringe. The low-frequency tilt signal is therefore in the PZTs, while the high frequency seismic tilt is in the PDs. The raw displacement signal is converted to angle by dividing by the arm-length (roughly 15 cm from the center). The beam-balance is also damped with capacitive actuators using the PZT control signals.
The fiber interferometers are operated with a large gap (using a collimating lens) and thus are individually limited by the frequency noise of the common laser. However, taking the difference of the PD signals allows us to subtract frequency noise to the extent that the cavity lengths are matched. Crudely,
PD 1 = Angle + L1 * Frequency noise
PD 2 = -Angle + L2 * Frequency noise
Therefore,
SUM = (PD1+PD2)/2 = Frequency noise*(L1+L2)/2
and DIFF = (PD1-PD2)/2 = Angle + Frequency noise*(L1-L2)/2
The attached plots show data measured this afternoon. The first plot shows the PZT and PD signals for each cavity. After the flexure replacement on Monday, the instrument is slowly settling but is continuing to drift in one direction as seen from the plot.
The second plot shows the ASD of these four signals. As explained above, the tilt at higher frequencies is in the PDs and the low-frequency tilt is in the PZTs.
The third plot shows the ASD of the SUM and DIFF channels. Note the smooth 1/rt(f)-ish slope in the SUM channel (at low frequencies) indicating that it is limited by the frequency noise, as expected. Unfortunately, there appears to be excess noise above 10 Hz, which look like acoustic pickup of some sort. This was taken during a noisy LVEA, so it is possible that after the clean room fans are turned off and it gets quieter, the noise will go down. The DIFF, does dip below the SUM as expected - indicating that we are getting some frequency noise suppression. It is not clear what the noise floor of the DIFF channel is yet. IF there is a factor of ~3 frequency noise suppression (at a minimum), then the noise floor ought to be a factor of 3 below the SUM channel (~ 30 picorad/rt(Hz) at 10 Hz). But if we are limited by acoustic noise, then the noise floor could be worse.
The fourth plot shows coherences between some interesting channels.
Compact BRS is performing reasonably well at the moment. Stay tuned for more data/plots when things are quieter. I'll also try to compare c-BRS with other local sensors.
I've attached some spectra recorded last night from 9:30 to 12:30 pm. I've also included the nearby STS-2 seismometer (ITMY STS) in veolcity units.
First plot shows the low-frequency spectra, which is very noisy below the resonance. This is likely all temperature noise and was expected as the instrument is not in vacuum. However, this is irrelevant for the high frequency sensititivity.
The second plot shows the DIFF (actual floor tilt) and SUM (~frequency noise) spectra along with the STS-Z. The floor of the DIFF spectra dips down to ~ 50 picorad/rt(Hz) at ~2.5 Hz and the bump there seems to be real, as it is seen in the STS as well. Unfortunately, the fans were still not OFF yesterday so many high frequency peaks are visible in both instruments.
Krishna
I measured the tilt transfer function (normalized to 1 at high frequencies) for Compact-BRS yesterday by driving it with a piezo stack located under it's platform. The drive would produce both rotation and vertical motion of the platform, but as d is expected to be small, only the rotational drive is relevant. The first pdf shows the response of the instrument compared to the drive at five frequencies - four to the left of the resonance and one to the right (used to normalize the TF). The resonance was at ~62 mHz and the measurement suggested a d = 100 (+/-10) microns. The error bars and limits are rough estimates and not exact. This sugggested an addition of ~3.8 grams to the upper mass to reduce d and obtain a final frequency of 47 mHz.
After a few attempts at trying to adjust the frequency (mainly due to inaccurate frequency measurements), I finally got it close to 49 mHz, which I deemed to be sufficient. The new transfer function measurement yielded the second plot, indicating d = 11 +/-2 microns. For this value of d, the translation rejection is given by M*d/I = 4.9 kg*11e-6m / (0.08 kg m^2) = 7e-4 rad/m.
This is much better than needed for high frequency (>1 Hz) seismic tilt measurement, where seismic wa5velengths are short and consequently the tilt (in rad) is substantial in comparison to the translaiton (in m) . At 10 Hz, for example, the wavelength is 20 m, therefore a translation amplitude of 1 nm has an associated tilt of ~ 0.3 nrad. A more patient and careful tuning process can reduce d below +-1 micron.
Opened exhaust check-valve bypass-valve, opened LLCV bypass-valve 1/2 turn -> LN2 @ exhaust in 16 minutes 20 seconds -> Restored configuration to as found. Next CP3 overfill to be Friday, Aug 12th.
On 8/8 I checked the PSL chillers, per work order 6482, and found that the crystal chiller was a bit low, so I added 100ml of water. The diode chilller was not in alarm, so I did not add water to it.
Summary:
Hugh, Jim
This morning Hugh and I went out and rebalanced the ISI. We removed some weight from the sides to compensate for buoyancy, something we missed last time. Now the ISI should have less DC drive in vacuum, before it was holding a 40 micron offset in Z, should be more like 10-15 now.
TFs were taken this morning, and other than missing the dewhitening setting on the GS-13s (HAM6 runs in low-low gain with dewhitening off to avoid tripping when the toaster pops) the TFs look the same as a measurement I took in 2014. Attached plots are GS13s, blue, brown, light blue are the current measurements, red, green and pink are the 2014 refs.
After hearding the cats to obtain each subsystems signature for closeout, we are now putting the doors (N, S) on HAM6. A film crew is looking on.
We removed two D071200-00s and four D071201s, a total of about 1.5 lbs. The table top payload and sidewall payload as-found and changes made are captured in D1201388 as-built file, loaded to the DCC.
WP #6069 To allow copying of raw minute trend files from the h1tw1 SSD RAID, the existing raw minute trend directory was renamed and a new directory created. This required restarting the h1nds1 daqd process to add the new directory path. This will need to be done again when the copying is completed.
Work Permits Summary, Maintenance Day 2016 August 9
WP Number | WP Date | Description | alog(s) or comments |
6052 | 08/03/16 09:35 PM | Activity: Separately power and move CPS timing distribution boxes. Possible comb source. | End station CPS timing fan outs running on separate power, BSCs re-isolated. Alog 28915 |
6053 | 08/04/16 02:38 PM | Activity: Add capacitor from HV stage to LV stage per ECR E1600230. This is to allow PI signals to work in both HV and LV states. This will take each end ESD down for hour or so each. Area of Activity: ETMx Low Voltage ESD driver | |
6054 | 08/04/16 04:48 PM | Activity: take ETM images using Pcal camera at EndY | |
6055 | 08/04/16 04:58 PM | Activity: Replace 20 in-air metallic mirrors on HWS X and Y table | |
6056 | 08/04/16 08:15 PM | Activity: Relocate existing fabric and add new fabric to wind fence at E X. Fabric will be placed 4' above ground level and extend up approximately 16' above ground level. This work will require the use of the LIGO outdoor boom lift. | |
6057 | 08/04/16 08:22 PM | Activity: Replace the batteries in the scissor lift that is located in the west bay of the LVEA. | |
6058 | 08/04/16 08:24 PM | Activity: Degas PT170 & PT180 Inficon wide range nude ion gauges, one at a time. | Alog 28927 |
6059 | 08/05/16 04:54 PM | Activity: After hours and weekend work in the LVEA and VEAs. This permit does not cover activities that would require a work permit during regular hours. A buddy system will be used for risky activities such as operating heavy equipment. Typical work includes investigations of environmental coupling, such as set up of sensors and injection equipment. | |
6060 | 08/05/16 05:55 PM | Activity: Bake RGA using manual variacs and heat tapes * RGA isolated from Y-end vacuum volume via closed 2 1/2" metal valve * RGA pumped by turbo which is bolted to the RGA assembly and which is backed by cart-mounted turbo which is then backed by free standing scroll pump * scroll pump and pump cart are strapped together and C-clamped to BSC6's stand weldment * Vent protection provided via an electropneumatic isolation valve mounted between the two turbos which closes upon a programmed pressure threshold or by a loss of power. A second spring/solenoid isolation valve is mounted at the scroll inlet and closes upon a loss of power * All pumps have vent valves removed and vent ports plugged | |
6061 | 08/05/16 06:04 PM | Activity: Finish surveying viewports on site to inspect hardware on viewport covers. | Alog 28928 |
6062 | 08/06/16 10:34 PM | Activity: Bake RGA using manual variacs and heat tapes * RGA isolated from Y-end vacuum volume via closed 2 1/2" metal valve * RGA pumped by turbo which is bolted to the RGA assembly and which is backed by cart-mounted turbo which is then backed by free standing scroll pump * scroll pump and pump cart are strapped together and C-clamped to BSC6's stand weldment * Vent protection provided via an electropneumatic isolation valve mounted between the two turbos which closes upon a programmed pressure threshold or by a loss of power. A second spring/solenoid isolation valve is mounted at the scroll inlet and closes upon a loss of power * All pumps have vent valves removed and vent ports plugged | |
6063 | 08/08/16 04:10 PM | Activity: Replace temporary Coil Driver for ITMX Corn2 with repaired original unit: De-Isolate ISI, swap CD Chassis, repower, reisolate. Duration ~1hr, blend w/ commissioners. |
H1 ITMX ISI Corner2 Coil Driver Original Unit Swapped back in. Alog 28948 |
6064 | 08/08/16 04:49 PM | Activity: Replace annulus ion pump on GV3. Ladders only needed. Area of Activity: LVEA VE GV3 AIP R&R | Alog 28965 |
6065 | 08/08/16 05:53 PM | Activity: Relocate HAM6 shutter controller from ISCT6 to ISC-R5 to eliminate the long cable run for the shutter trigger. Change R23 from 26.7K ohms to 12.4Kohms in the QPD transimpedance amplifier chassis. This is to increase the maximum threshold for the AS port trigger PD as seen by the shutter controller. See alog https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=28909 | |
6066 | 08/09/16 03:44 PM | Activity: This task is to finish the timing upgrade. This includes the Master, Fanouts and any comparitors that might have been missed. This will require a full restart of all Computer and IO chassis. | Alog 28967 |
6067 | 08/09/16 03:45 PM | Activity: remove extra binary io card from chassis. Area of Activity: H1SEI 16 adn h1sei23 | done, card installed in psl for ISS 3rd loop work alog 28967 |
6068 | 08/09/16 05:40 PM | Activity: (The following work to be performed while leaving the Vertex RGA isolated from the Vertex Vacuum Volume via a closed 2 1/2" metal valve) * Bag RGA assembly * connect and run leak detector (LD) * valve-in LD to RGA volume * Open Cal-Gas isolation valves * evacuate bag (at bottom) with O2 sensors (w/internal pumps) while filling bag (at top) with helium * Restore configuration to as found when complete. Area of Activity: Vacuum, Vertex RGA, LVEA | Alog 28964 |
6069 | 08/09/16 09:52 PM | Activity: Copy minute_raw files from h1tw1 SSD RAID to /frames/trend/minute_raw. Once files are copied, remove them from the SSD RAID. This is routine maintenance. Will require a restart of h1nds1 daqd at the start of the copy and again at the end to allow continuous access to the data. Area of Activity: h1tw1, h1nds1, control room. | |
6070 | 08/09/16 11:15 PM | Activity: Lead film crew for shoots in LVEA, roof, control room and possibly sites outside (e.g. overpass). Nominally 6am - 6pm, with the early start to avoid commissioning. |
Found the FSS AUTOLOCK was oscillating. Could not adjust the gain due to Guardian control. Per Jason: (1). Took the Guardian node PSL_FSS to AUTO (2). Set the state to IDLE (3). Adjust the COMMON GAIN to 16dB (4). Set the state to READY_FOR_MC_LOCK Jason and TJ are looking into an elegant long term solution.
I did a few things today.
1) Updated the final FSS Common Gain to its new value of 16 (previously 20).
2) Rather than just throwing in the new gain when the FSS is no longer oscillating, it will make four steps for one second each to get there. If the FSS begins to oscillate while it is stepping, then it will start over when the oscillation is done.
I tested it a bit and all seemed well, but if there are any issues then just go back a revision.
Topped off the Crystal Chiller to 155mL (it seems whenever I took it to the MAX level, it would immediately drop. So I took it to max twice and called it good....and then it dropped.)
Diode Chiller had no alarm.
[Corey, Betsy, Fil, Peter, Calum, Stefan, Koji]
Summary
- The ISC portion of the HAM6 vent work has been completed.
- Shield isolation of the in-vacuum cables was confirmed.
- The fast shutter was reinstalled on the table after some modifications.
=> Ready for the SEI mass balancing and other exiting procedures. OMC PZT HV is still on. Remeber to turn it off before pumping down.
Some details
- Shield isolation: It is always confusing to check the shiels isolation on HAM6 because of several reasons.
We initially had several cables shorting to the chamber but all of them but one happened at the slack of the cables right inside of the flange. The last one happened on the DB25 cable before it climb up to the vertical wall of the ISI.
- The fast shutter modification / reinstallation
(Photos are supposed to come later.)
Photos From Yesterday's Fast Shutter Work
Photos are on Resourcespace here:
https://ligoimages.mit.edu/?c=1705
Cable Grounding Check
(Corey, Fil, Koji)
Documents of interest:
We went through as many of the ISC/SUS cables as we could, which is mainly all the DB25 connectors (most were on a single flange, D6). The non D6 cables [i.e. SUS OMC & WFS Heads] were checked at the CDS rack (east of HAM6) & the SUS rack (south west of HAM6). We did not check the RF WFS cables at D5 (not sure how to make check on these connectors, and Koji was worried about disconnecting the connectors since it could make things worse. We also did not check SEI since those cables were not touched and are nicely clamped & out of the way.
Some notes:
OMC Cables (D6: F1, F2, & F3): These cables all go to a harness on the OMC breadboard. Their sheilds are all tied to each other. Since we checked these cables at the flange, You must disconnect all three cables at the same time. Then you can do the ground loop check (otherwise, if you do one at a time, you will trick yourself into seeing ground loops, but this is because their sheilds are all connected).
For the Picomotor cables, I thought Koji said we should disconnect the cable from the picomotor and then check for grounding, but I can't remember if that is really necessary.
Bird's Nest!: We found some shorts. When one finds a short, the job is to go in chamber and then "wiggle" the cable in question until you no longer see the short. I believe we were able to do this in-chamber right next to the D6 flange. This is where there is a "bird's nest" of ISC cables (unfortunate...I reckon we could clean this up by carefully clamping ISC cables down to HAM6's Stage0.).
At any rate, whenver one fixes a cable with a ground loop, one must then re-check all cables! This is because all these cables are in this "bird's nest". And if you remedied one by moving it around, you don't know whether you made things worse for a neighboring cable in the "nest".
At the end of the day, we were happy with our ground loop checks for these cables.
OH, a To Do Item:
At the D6 Flange, it was easier for Fil to plug/unplug cables when he removed some protective bars were removed from the flange protector. At the nearest convenience, those bars should get re-installed.
Re the To Do Item--removal of the 'protective bars' aka strain relief, to make it easier to unplug cables. These should be replaced and returned to relieving strain by the remover. There is plenty of instances where this has not been done and I expect is the SOP, sadly. The job is always so much easier if you don't have to return to it later, after you've remembered it.
> For the Picomotor cables, I thought Koji said we should disconnect the cable from the picomotor and then check for grounding,
> but I can't remember if that is really necessary.
No. It turned out that the picomotors have no shields at the mighty mouse connectors and have no shorting the the table.
HAM6 CC wafer placement - it is now back in the same place as the last one was pulled from.
Bubba, Jim, Dave:
UNIT-1 cooling in the MSR developed a very noisy fan this afternoon. It has been opened as FRS-6039. This system was turned off and the other two units had their set points reduced from 70F to 67F after the room became noticably warmer.
The room temperature can be monitored via the Beckhoff channels H1:pEM-C_MSR_RACK[1,2]_TEMPERATURE. It shows the temp increased from 18C to 26C (64F to 78F).
With the system at 80degF last night I had Tara open the door to the room to get some cooler air in. Seems to have stabilized the temperature.
This morning Bubba lubricated a bushing and has started the fan back up. If the noise starts again we will have to shut it down again. Bubba is looking into a replacement motor.
I was taking some measurements on the BSCs earlier today, and I noticed a feature at about .73 hz in the OAF CARM and DARM suspoint channels that didn't show up in the OAF MICH suspoint spectra. I then looked at the GS13s on ETMY and there is a pretty sharp feature that seemed to have appeared after recovery this morning. A quick cruise through the Summary pages, though, showed that there is some intermittent feature that has been there off and on since at least the end of June. I thought it might be the RX/RY loops on ST2 I've been trying, but turning those off had no effect. I then took the ISI St2 to damped, but the feature was still there. Jeff said that the TMS has a resonance about .73 hz, so I turned the damping off and that made the feature much worse, but it also rang up a bunch of other features. Whatever this is, it has to be very intermittent since I hadn't noticed it before today, and I look at ETMY pretty frequently, and I've never noticed it before.
Attached plot is the ST2 RX GS13, which showed this the strongest, though RY and Y also saw it. The CPS also saw this in all configurations, even damped. The TMS sees this, though not as big, and the quad sees even less and only in pitch. ST1 of the ISI does not see this.
For future reference, recall that H1's TMSY is the only "first article" TMTS, slightly different from every other "production" TMTS. The mode that is close to this frequency is modeled to be at 0.734 Hz. *If* this resonance is the source of the feature seen in the ISI, I suspect the coupling to ST2 rotational DOFs is because the TMS is mounted far from the center of the optical table. I've taken a damped and undamped transfer function this morning to confirm that this mode is "well" damped when damping loops are on. RED is current damped BLUE is current undamped and BLACK is some previous test in June of 2015. Indeed, the undamped resonance is at 0.73 Hz (and there's actually a cluster of three resonances from various other modes cross-coupling into the measurement), but as the damped measurement confirmed, the Q is a low ~15-30, as designed.