This week:
Week 4/4:
J. Kissel Joe Betzwieser has created some new bit of "user" c-code in order to facilitate getting the ISI's GS13s, projected into SUSPOINT longitudinal, to the corner station to be further projected into the IFO's cavity length basis. The code serves to mux multiple low-sampling rate channels (in this case, SEI channels) into one high-sampling rate channel for shipping over the RFM IPC with less overhead. See T1600083 for details. To absorb this new code for incorporation into the PEM model (as per the plan, see LHO aLOG 26249 and ECR E1600028), I've updated the ${userapps}/cds/common/src/ directory of the local copy of the cds_user_apps repository. -------------------------- Exactly what has been received: jeffrey.kissel@opsws2:/opt/rtcds/userapps/release/cds/common/src$ svn up A LOW_FREQ_MUX.c A ccodeio.h A MAX_MIN_CALC.c A LOW_FREQ_DEMUX.c Updated to revision 12938. jeffrey.kissel@opsws2:/opt/rtcds/userapps/release/cds/common/src$
Pressures still falling: HAM 7/8: 5.6e-6 Torr (Friday=8e-6 Torr) HAM 9: 3.8e-6 Torr (Friday=6e-6 Torr) HAM 11/12: 3.5e-6 Torr (Friday=5e-6 Torr) Then turned available annulus IPs ON: HAM 8: 7 mA (pressure at cart jumped to 9.6e-6 Torr) HAM 9: full scale with red light (pressure at cart jumped to 5.5e-6 Torr) HAM 11: full scale with red light (pressure at cart jumped to 4.2e-6 Torr) Need power and signal cables for IPs on HAM 7 & 12. Power cord on HAM 8 is sketchy with tears in outer insulation. I've asked Phil to replace it. Continue to monitor pressures to detect any potential outer o-ring leaks.
Michael, Krishna
Yesterday, we tested some soft rubber-like pad under the turn-table to reduce the impact of the vibrations in the BRS-1 damper (as discussed here). This was unsuccessful and today we went back to the previous configuration with some thin sheets of closed-cell foam. The arrangement works for now but will likely not be permanent.
BRS-2's vacuum can was completely closed yesterday and we hooked up the portable pumping station to it but couldn't figure out how to enable the safety interlock to start pumping. We will start pumping on Monday after talking to the vacuum experts. We also connected the Satellite box to the Beckhoff computer and the 24V DC power supply. No issues there.
The high freqency calibration lines injected at the end of O1 (alog 24843) were analyzed to estimate the sensing function at those frequencies and compare it to the matlab DARM model. The calibration at frequencies above few kHz shows deviation from the model. The upward trend in the residual, as shown in the plot below, looks like the effect of the bulk elastic deformation of the testmass due to the misalignment of the pcal beams. However, this is not a definitive conclusion because the phase doesnot seems to suffer so much and also the error bars are too large to make a definitive statement. A set of measurement might be necessary to see if this effect is in fact reproducible.
The SLM tool was used to estimate the line amplitude with FFT duration listed below for each individual lines. The mean of the several data points was taken as the central value and the coherence of the measurement was estimated using magnitude squared coherence:
Coh = (A.B*)2 / A2 * B2
where A and B are amplitude of DARM_ERR and PCAL_PD channels readout.
Freq Amplitude Start Time Stop Time Duration FFT Data points Optical Gain (Hz) (ct) (mm-dd UTC) (mm-dd UTC) (hh:mm) (mins) (#'s) (kappa_C) ------------------------------------------------------------------------------------------------------------------------------------------ 1001.3 35k 01-09 22:45 01-10 00:05 01:20 10 8 0.995 1501.3 35k 01-09 21:12 01-09 22:42 01:30 10 9 0.995 2001.3 35k 01-09 18:38 01-09 21:03 02:25 10 13 1.00 2501.3 40k 01-09 12:13 01-09 18:31 06:18 30 12 0.995 3001.3 35k 01-10 00:09 01-10 04:38 04:29 30 8 0.99-0.96 (Fluctuating) 3501.3 35k 01-10 04:41 01-10 12:07 05:26 30 10 0.99 4001.3 40k 01-09 04:11 01-09 12:04 07:55 60 5 1.00 4501.3 40k 01-10 17:38 01-11 06:02 12:24 60 11 0.99 5001.3 40k 01-11 06:18 01-11 15:00 ~9:00 60 9 -----
These additional data points were added to one of the Pcal sweep done earlier during the run. In this case I picked the data from 2015-10-28. The optical gain during this sweep measurement was around 0.985 compared to 0.99-1.00 (from table above) during the high frequency injections. These optical gains were eye-balled from the detchar summary pages so I considered them within the margin of error and thus didnot do any correction. A new parameter file is created to run this as a new set of measurement. The parameter file is stored at the following location:
ligo/svncommon/CalSVN/aligocalibration/trunk/Runs/O1/H1/Scripts/DARMOLGTFs/H1DARMparams_20151028E.m
A script used make the plot attached above and save the output as a mat file is located here:
ligo/svncommon/CalSVN/aligocalibration/trunk/Runs/O1/H1/Scripts/DARMOLGTFs/make_sensing_HF.m
The result of the the above script is saved at the following location and is also attached to this alog.
ligo/svncommon/CalSVN/aligocalibration/trunk/Runs/O1/H1/Resulta/DARMOLGTFs/2015-10-28E_H1DARM_HF_sensing.mat
Hi Sudarshan,
Does your model include the FSR peaks ? In other words, it the DARM sensing a single pole model ? See, for example, G1501316.
In the attached figure we show the effect of the test mass deformations due to PCal beams on the calibration using COMSOL simulations. For the simulation we used the locations of the PCal's beams from T1600372 and main beam from G1501362 . The two curves in the plot corresponds to maximum and minimum offsets of the beams that we get from these documents. Explicitlly for the main beam we used (5,-5) mm and for PCal beams we usedd the values reported in the table below.
MAX OFFSET [mm] | MIN OFFSET [mm] | |||
X | Y | X | Y | |
Upper beam | 1.8 | 6.1 | -0.2 | 4.1 |
Lower Beam |
1.77 | 6.6 | -0.23 | 4.6 |
We normalized the data points so that it will be 1 at low frequencies (the normailzation was 0.983).
1500 - 1510 hrs. local -> To and from Y-mid Exhaust check valve bypass opened, LN2 at exhaust after 2:47 mins with LLCV bypass open 1/2 turn Next CP3 over-fill to be Tues. before 4:00 pm hrs. local
Daniel, Ed D., Ross, Dave B., Terra
In anticipation of more parametric instabilities as we go to higher power, we've set up the ESD PI damping scheme here (which has been successfully used at LLO so far).
Brief context: Figure below shows example relationship between blue mechanical modes of test masses and red optical TEM00 and TEM03 beat note peak (seen at LLO during O1; figure courtesy of Carl Blair). As red optical beat note peak moves left or right, it overlaps with the mechanical mode groups on either side, which can lead to PI. Each mode group has 4 peaks, one for each test mass. Simulations of surface deformations for each mode are shown near their respective peaks. Previously at LHO, PI was observed near 15540Hz and the ETMX ring heater was turned on, effectively moving the red peak leftward away from the 15540 mode group and towards the stable region as shown below. However, as we increase power, high mechanical mode density will mean smaller stable regions to tune towards; hence the need for an active damping scheme.
Work this past week: ESD damping scheme is set up and ready for testing.
We've updated end station pi models (h1susetmxpi, h1susetmypi) and added a corner station pi model (h1susitmpi) to allow for ESD driving; these now match LLO's PI models, with some extra downconversion options added. Note that LHO currently doesn't have ITM ESD drivers, so corner station model is just in anticipation.
I've overhauled the X and Y-arm PI medm screens (screenshot attached), located in userapps under /sus/common/medm/pi. For now, only X and Y arm PI screens exist - orange PI buttons on main sitemap. Screens shown in screenshot unfold clockwise from top left for ETMX. Main screen holds list of modes that will be identified over time. Each mode then has its own screen for it's damping parameters.
The basic damping scheme for the ETMs is as follows: Arm transmission QPD signal carries test mass resonant mode information. QPD signal is passed through an analog 10K - 80K filter (see D1400419 for a rather enlightening PI hardware diagram). The 4-segment QPD vector is multiplied by INMTRX which selects for vertical or horizontal mode orientation. Band pass filter bank to pick out mode frequency; usually 2 x tight bandpass of <10Hz. Control filter bank to damp; gain of 100+, gain of -1 to damp, double zero1, pole 1000. All are shown in attached medm screenshot. Finally, PI has actuation control on two LNLV ESD drive segments: UR & LL.
We're also temporarily recording the OMC DP PDs at 64K at H1:OMC-PI_DCPD_64KHZ_A and _B as these have the best SNR for PI modes (via the new h1omcpi model). After the ring heater test (discussed below), we'll change these to record at a slower rate.
To do: There wasn't an available long lock > 10W while I was here so there's some testing of the system still to do.
1. Test ESD damping on known mode: As mentioned above, PI was previously seen at LHO at 15540Hz in ETMX at 15W. It was successfully avoided by turning the ETMX ring heater on; it has remained on since then at 0.5W requested power upper and lower. In an upcoming longer lock at ~15 W, the ring heater should be turned off to allow the 15540 mode to ring up and attempt to be damped with the new ESD scheme.
2. Ring heater test: To match mode to test mass, we can step up the ring heater on each respective test mass and watch which PI mode shifts in response. We need to step up one ring heater at a time by 0.1 W (both top and bottom simultateously) for 10-15 minutes each.
3. Implement line tracker before damping filter: Ed and Ross have been working on a line tracker that will lock onto each somewhat-well-identified PI mode. It's in the last stages of testing and will be added to the model and sitemap (in between the BP filter and damping filter) asap. Ed & Ross have a more detailed alog about this in the works.
The response of the TM ROC is given in the TCS SIMULATION. (For ETMX, for examplel, H1:TCS-SIM_ETMX_SURF_DEFOCUS_RH_OUTPUT and the full ROC is in H1:TCS-SIM_ETMX_SURF_ROC_FULL_OUTPUT).
We measured the response of the ROC to the RH back in the One Arm Test. See page 9 of T1200465.
The frame writers became unstable after the PI model changes Thursday 24th March. Attached is a plot of their restarts since that time. Initially fw0 was unstable, it then became stable and fw1 went unstable for periods of time. Note the regularity of h1fw1 restarts, roughly every hour around the 30 minute mark, with occassional restarts around the 45 minute mark.
The hourly restarts around the 30 minute mark have been correlated to the hourly running of the wiper script (crontab starts this at 23 minutes in the hour, it finished around the 30 minute mark). I was able to correlate this by changing the crontab time from 23 minutes to 03 minutes at 10:40 today. From that time onwards the restarts happened around the 10 minute mark. h1fw1 restart times for today are:
27_Sunday_March_2016_14:06:49_PDT
27_Sunday_March_2016_13:08:09_PDT
27_Sunday_March_2016_12:11:29_PDT
27_Sunday_March_2016_11:08:50_PDT
27_Sunday_March_2016_10:45:11_PDT
--------------------------------- cronjob changed 23 to 03 minutes
27_Sunday_March_2016_10:29:01_PDT
27_Sunday_March_2016_09:30:52_PDT
27_Sunday_March_2016_08:28:12_PDT
27_Sunday_March_2016_07:44:03_PDT
27_Sunday_March_2016_07:30:23_PDT
27_Sunday_March_2016_06:27:18_PDT
27_Sunday_March_2016_05:42:08_PDT
27_Sunday_March_2016_05:27:59_PDT
27_Sunday_March_2016_02:28:18_PDT
27_Sunday_March_2016_01:28:08_PDT
27_Sunday_March_2016_00:26:28_PDT
This suggests SAMFS disk access or NFS file sharing as a possible cause of the problem. I'll work with Greg and Dan tomorrow to see what diagnostics we can run on these file systems.
opened an FRS ticket, #5221 https://services.ligo-la.caltech.edu/FRS/show_bug.cgi?id=5221
Ed, Ross, Terra, Jim, Dave
we have added code to the x1fe3tim16 model to test Ed's line isolation C-code. When this testing is complete, we will run the code on other test models running at different rates.
We installed the boot disk Keith provided into a new boot server called x1boot1. Thats to Keith's extensive prep work, the install was very quick. We moved the fast front end computer x1susey from the 2.6 boot server over to the new 3.0.8 server. Next tasks are to rebuild the models on this machine.
x1susey ~ # uname -a
Linux x1susey 3.0.8 #3 SMP Wed Mar 9 16:13:18 CST 2016 x86_64 Intel(R) Xeon(R) CPU E5-2690 v2 @ 3.00GHz GenuineIntel GNU/Linux
We did a little bit of ASC work today.
First, while Kiwamu was running a TCS test I started a script to automate phasing of the WFS. It uses the lockin, first runs a servo to set the phase of the lockin demod, then servos to minimize some signal. We have it set up right now to phase the refl WFS to minimize the PR2 pit signal in Q for both REFL 9 and 45, and to minimize the SRM pit signal in AS 36 Q. There is some code for exciting DHARD, but we need to test amplitudes, phases and gains for this. The current version of the script does its job although it is painfully slow, and is checked into the svn under asc/h1/scripts THe resulting phases are in the attached screenshot.
We saw that the instability in CHARD pit was becasue somehow the LP9 got turned on again, this is now off and CHARD seems fine.
We tried powering up, were fine at 10 Watts. We had an instability in PRC1 and PRC2 yaw at 13 Watts. I reduced the Q on the complex zeros at 1.1 Hz for PRC2Y, which gives us slightly better phase and gain near the point where we seem to be unstable. Attached is a screenshot of the OLG measured with white noise at both 2 Watts and 10Watts, we might need to do a swept sign to get a good measurement around 1 Hz.
After about 10 minutes at 12 Watts, we had the usual fluctuations in the recycling gain. So the high bandwidth PRC2 loops haven't totally solved the problem.
For the record, these are angle settings that give approximately good CO2 powers tonight, and the powers to aim for from Kiwamu's note:
X power (W) | X angle | Y | Y angle | |
unlocked | 0.5 | 76 | 0.23 | 82 |
10W | 78 | 79 | ||
20W | 0.3 | 0.1 |
We have twice had the rotation stage for CO2 Y go to an angle that was wrong by a lot (sending a few watts to the test mass for a few seconds).
I'm leaving the IFO locked at 10Watts.
Sheila,
Do you know how much power was transmitted at CO2 Y to any precision? Can you say what the upper limit was?
thanks
The first time H1:TCS-ITMY_CO2_LSRPWR_MTR_OUTPUT read back 3.2 Watts for about 20 seconds.
THe second time H1:TCS-ITMY_CO2_LSRPWR_MTR_OUTPUT read 3 Watts for about 10 seconds.
This morning I looked at some of the data from friday night when we had our usual CSOFT instability. (16-03-26 7:52:56 UTC)
First, I used the moment of interia here, and the calibration of the arm circulating power from the transmon QPDs here, to estimate i it is reasonable that radiation pressure due to the fluctuations in arm circulating power (on the order of 2.5% fluctuations on 35 kWatts of circulating power) could cause the angular motion that we see (0.1-0.4 urad pp on the test masses), and it is not, the miscentering that would be required is far too large.
I never attached the sreenshot of the PRC2 Y OLG to the original alog. Here it is.
TITLE: 03/26 Eve Shift: 00:00-08:00 UTC (16:00-00:00 PST), all times posted in UTC
STATE of H1: Planned Engineering
INCOMING OPERATOR: None
SHIFT SUMMARY:' Large tour group in the control room. Got a chance to really talk at length with some guests about my job and a little bit about various subsystems with a camera guided tour around the LVEA. Completed the last ofthe Sat Amp modifications. Did a little bit of re-locking for Sheila. She's going to be working on DRMI/TCS relationships for the remainder of the night.
LOG:
23:21 Chandra back from CP3 refill
00:15 Terra and Nutsinee to EY to do some signal injections
0:46 Terra and Nutsinee back
Michael, Krishna
This morning, we repositioned the EX_BRS-1 damper turn-table and restarted EX_BRS-1 software. The system worked normally and started to damp the balance but was unable to damp it all the way to small amplitudes (< ~50 counts/nrad). The reason seemed to be that the turn-table vibrations were driving up the beam-balance (see here). Looks like the foam sheets under the turn-table aren't effective at vibration damping any more. Later, Hugh handed us some soft polymer damping pads which we'll try out tomorrow. In the meantime, I've disabled the damper but the tilt data is available.
At EY, Carlos helped us to get the autocollimator software (in C#) working on the BRS-2 Beckhoff computer. We then proceeded with the vacuum can assembly and then aligned the autocollimator and adjusted the beam-balance position to get clear images on the CCD. By the end of the day, the angle data of the beam-balance was visible on the Beckhoff computer.
Plan for tomorrow:
1. Try out other vibration damping pads under the BRS-1 turn-table. Also try out some BRS-1 code changes to improve the software live-time, which crashes once in ~two weeks.
2. Continue BRS-2 vacuum can assembly. If possible, start pumping the vacuum can.
3. Hook up the SEI-Interfacing beckhoff modules.
This is a quick summary of today's TCS joy. I ran another differential lensing test today. I went to the other side of the differential lensing (CO2X goes higher power).
The highest cavity pole was 352 Hz in this test.
This time, I also took many measurements of the intensity and frequency noise couplings periodically throughout the test using Evan's automated measurement script (20470). I will analyze and post them later. The second attachment is trend of some relevant channels.
This is a report on the intensity noise coupling measurement to DARM during the same TCS testing period.
The below is an animated plot showing how the intensity noise coupling evolved as a function of time during the test. The transfer function was measured from ISS-SECONDLOOP_SUM14_REL to CAL-DELTAL_EXTERNAL. DELTAL_EXTERNAL is unwhitened.
As shown in the above animated plot, the intensity noise increased at the beginning and then went back down to where it was. The overall spectral shape almost did not change, but the scaling factor has changed roughly by a factor of two comparing the minimum and maximum. The magnitude of the coupling rises in proportion to frequency -- if I plotted them for a coupling to DCPDs, they would be almost flat due to the cavity pole correction taken out.
Here is another plot showing the evolution of coupling as a function of time.
The upper plot shows the transfer coefficient at 2500 Hz (in arbitrary unit) as a function of time. The bottom plot shows the CO2 lensing from the same period. The transfer coefficient shows a clear correlation with the defocus of ITMs. I can not say for sure if the differential was a dominant cause of this effect because I had a few uD defocus as well in the same fashion.
Here is the same analysis for the frequency noise coupling to DARM. The variation in the coupling is more drastic than that of intensity noise.
The below is a same type of animated plot. The transfer function was measured from REFLA_RF9_I_ERR to CAL-DELTAL_EXTERNAL. Note that DELTAL_EXTERNAL is properly unwhitend.
It seems that the coupling has two different mechanisms, one for the coupling below 300 Hz and the other for the above. As the CO2 setting changed, the high frequency part increased at the beginning and decreased later while keeping the same spectral shape. On the other hand the low frequency part varied in an opposite fashion; it decreased as the high frequency part increased. The slope of the high frequency coupling seems to be almost proportional to f. If we convert it into [OMC DCPDs [A] / laser frequency [Hz]], it will be more like 1/f due to the cavity pole and REFL's transfer functinon against the laser frequency.
Here is another plot showing the evolution of the transfer coefficient at 2500 Hz. The coupling coefficient changed by a factor of 15 at this frequency. This is much more drastic than that of the intensity noise coupling which varied by a factor of two or so.
A preliminary conclusion:
With the 2 W PSL, the DARM cavity pole prefers a high CO2 differential lensing while the laser noise couplings prefer a low differential lensing.
This is a belated analysis on the intensity noise coupling. The punch lines are:
[Noise coupling v.s. differential lensing]
As seen in the plot above, the coupling coefficient shows a linear relation to the differentianl lensing. This likely indicates that the differential lensing is not optimized to minimize the intensity noise coupling. I should note that this measurement had used the badly clipped COY beam (27433) which was later fixed in May 2016; a smaller differential lensing means less power in CO2Y than CO2X.
[Intensity noise coupling]
Here is a plot showing the intensity noise coupling of the various TCS settings. This time the coupling coefficient is converted to OMC power [W] / input RIN. The dashed line in the magnitude represents the expected value calculated by
(coupling) = 2 * J1^2 * Pin * Tomc * Tifo [W/RIN] = 5.5e-6 [W/RIN],
where Pin = 2 W is the PSL input power, Tomc = 61.4 ppm is the OMC transmission for the 45 MHz RF sidebands, and Tifo is the transmission of the intereferometer for the 45 MHz RF sidebands which I have assumed to be 1 for quick calculation. As seen in the plot, the expected noise level (limited by the 45 MHz RF sidebands) is lower then the measurement by roughly a factor of 10. These two plots support the hypothesis that we are far from the optimum point.
Here are the beamsplitter angles as a function of differential lensing. (There are some data dropouts in the trends).
This seems to indicate that a differential lens change of a few tens of microdiopters causes the beamsplitter yaw to change by a few hundreds of nanoradians, presumably via changes in the 36 MHz angular plant. In pitch it is less clear whether we are seeing angular control effects or simply drift over time.
In today's HAM6 vent meeting people asked if the shutter was working at all. It still works.
The first attachment shows that the shutter closed (green trace) last night when the IFO lost lock. Brown is the tirigger voltage, and the trigger threshold is 2V.
Red is the OMC DCPD, blue is the DC of ASAIR_A, vertical lines indicate where the shutter triggered.
Due to some strange timing problem of Ethercat signals transported to EPICS that was reported in alog 17445, you cannot compare the timing of the green and the brown trace with red and blue, so the trigger timing on this plot is just a guesstimate obtained as follows:
The second plot shows that the shutter has been firing all the time for recent 100 days.
One thing that is strange is that the LSC-ASAIR_C_LF_OUT_DQ is recorded on the frame at 16kHz but the input is grounded in the frontend. If my memory is correct Dan Hoak wanted to record the trigger voltage at 16kHz, and my guess is that ASAIR_C_LF was supposed to be used for this because it's not used, but nobody implemented it.
Preliminary conclusion: the DARM cavity pole seems to be a strong function of the differential lensing. I was able to change it from 357 Hz to 220 Hz (!!!)
I will post more details tomorrow.
The cavity pole measurement is not valid until t=80 min. and also in the time band approximately between 230 and 250 min. The interferometer was locked on the DC readout with ASC fully engaged, The PSL power stayed at 2 W throughout the measurement.
Learning this behavior, I would like to do the followings in the next test:
By the way the second attachment is trend of various channels during the test.
Actually, Hang pointed out that SRM and SR2 showed much more visible reactions in their alignment. See the attached.
In particular, SR2 pitch seems to trace the lensing curve.
Also, looking at PRM and PR2, we did not see drift or anything interesting.
A simulation with substrate lensings as reported in the elog did not show a large variation of the cavity pole: about 1% or so. My suspect is that the change in differential lensing is causing the IFO working point to change: alignment or longitudinal offsets? In my simulation the longitudinal working point is obtained from simulated error signals, so I don't see any offset in the locking error signals.
The differential lens change is about 18 microdiopters. For what it's worth, there is ~2.3% of power scattered from the TEM00 mode on a double-pass through such a lens. Whether such a purely differential lens in the SRC would manifest solely as a 2.3% round-trip loss in the differential TEM00 mode of the arms is questionable. I still need to run the numbers for the effect on the DARM cavity pole if we simply added this loss to the SRM mirror.
Here are some more small points to note.
[Two cavity pole measurements]
At the beginning of the run before I started changing the CO2 power, I ran a Pcal swept sine measurement in order to get the cavity pole frequency. The DARM open loop was also measured within 10 minutes or so in order for us to be able to take out the loop suppression. In addition, I ran another pair of Pcal and DARM open loop measurements to double check the measurement. The attached below shows the transfer functions with fitting. The fitting was done with some weighted least square algorithm using LISO.
As shown in the plot, the shift in cavity pole is obvious. Also the optical gain is different between the two measurements.
[Evolution of the sensing function throughout the test]
The optical gain and cavity pole are negatively-correlated. The trend of the optical gain looks very similar to the one for the power recycling gain, but the variation in the optical is much larger-- the optical gain increased by 20 % at most relative to the beginning. As pointed out by Valera in the ISC call today, a fraction of the variation in the optical gain could be due to the OMC mode matching.
[Alignment drift]
As Gabriele pointed out in the comment, it may be possible that the CO2 lasers affected the alignment of the interferometer and changed the amount of losses in some parts of the interferometer or introduced some other impact on the cavity pole. Hang and I have looked at trend of optical levers during the time.
There are two optics that seemingly reacted to the differential lensing, that are BS yaw and ETMX PIT. The showed a kink point at the time when the CO2 power changed. In addition, ETMY pit slowly drifted by 2 urad and ETMY yaw moved by 1-ish urad. Other large optics also moved but were within 1 urad. From a naive point of view, the alignment does seem to explain the behavior of the cavity pole going down and up during the measurement because none of them clearly showed a going-up-and-down type behavior. However, it is possible that the true misalignment was covered by drift of the oplev itself.
[Online cavity pole measurement]
The cavity pole was measured by injecting a line at 331.9 Hz at the DARM output. The DARM loop is notched out at the same frequency. The measurement method is described in 18436.
Some simulations I did months ago for the MIT commissioning meeting (https://dcc.ligo.org/LIGO-G1500593) showed that the cavity pole is very sensitive to SRC matching. I therefore expect the cavity pole to be also very sensitive to SRC alignment, as seems to be sugegsted by the SR* mirror drifts.