We have seen that the arm cavity can sometimes lock quite stably (for example the 6 hours starting UTC Jan 24 1:40) alog 9518, and that sometimes it mode hops constantly (alog 9653). I used the scripts Keita used in alof 9653 to make a comparision of the two times. For the stable time I am using 20 minutes of data starting at 1/24/14 1:40 UTC, for a bit less stable time I am using 1hr 20min starting at 1/24/14 6:30 UTC and a slightly less stable time of Keita's plots use 5 minutes of data.
First histograms of the transmitted counts: the stable time, the somewhat less stable time, and Kieta's data:



On the 24 (first two plots) the SHG was off, so there is no 850-900 count offset on COMM_A_LF that you see in Keita's data from this morning. The transmitted power this morning was only 80% of what it was durring the stable times, even when locked to the 00 mode (if you take into account the offset from the SHG).
You can see that there was mode hopping in Keita's data. Although it seems like the "less stable" (middle) histogram has a bimodal distribution, I don't think that the small hump aroung 550 counts is due to mode hopping because it has about 80% of the power that the 00 mode has. The mode matching should not have changed between the 24th and today, and we know we didn't have more than about 30% of our power in mode mismatch (alog 9518). These are most likely drops in the transmitted 00 mode power due to alignment excursions.
Here are plots of where the PIT oplevs spent most of their time, made using Ketia's script. This morning there was about 2-3 times more pitch motion in the ETM than on the 24th (see Jeff's alog).
These are plots made using Keita's script, of the transmitted power for different oplev positions. (I didn't use the threshold to distinuish mode hopping since there isn't really mode hopping in the first two plots, and I used a smaller bin spacing of 0.1urad) In the first two plots, we seem to be exploring a plateu where the transmitted power doesn't change dramatically over 1urad in ETM pitch and 1/2 urad in ITM pitch. This morning though we were misaligned, and even with less optic motion we would have been right on the edge of the mode hopping. It seems as though we can't rely on the dither alignment when we are this misalinged, and need to tune up the alignment by hand, probably by unlocking and watching the fringes.
The first two plots suggest we can stay locked to the zero zero mode with around 1 urad pp in the ETM, maybe more. The plot from this morning seems to show that while the optic motion was large, our main problem was a DC misalingment.
[Yuta, Paul]
This afternoon we set up the hardware for the IMC sideband sweep measurement, and took a test sweep of two cavity FSRs. This is in preparation for running automated sideband sweeps while stepping up the input power to get an estimate of IMC optics absorption (see e.g. LLO alog entry 9095).
First we checked the centering of the REFL beam on the in-vac LSC diodes, adjusting PRM alignment for this purpose.
Then we re-aligned the path from the ISCT1 REFL periscope to the in-air REFL diodes, after I misaligned it earlier when doing beam size measurements. Next we connected the Agilent network analyzer source directly to the 45MHz EOM input, without using the 18.8dB RF amplifier that was used last time for this measurement (see LHO alog entry 8098), and connected the 27MHz channel from REFL_AIR_B (broadband PD on ISCT1) to the network analyzer input.
Initial observations of the transfer function from N.A. drive into the EOM to a.m. measured by REFL_AIR_B around the 45.5MHz FSR showed the expected split peak structure (see LHO alog entry 8086). We then put a razor blade beam dump partially in the beam in front of REFL_AIR_B to break HOM symmetry at the PD. We misaligned the IMC to increase the HOM content injected, and then took a sweep across 2 FSRs from 36MHz to 55MHz. At some point during this process we noticed that the TEM00 peaks got much bigger, and also ceased to exhibit the split structure (see attached plot). Discussing this with Kiwamu later it appears that the IMC length shifted somehow during this time, giving a lot of a.m. in transmission with the previously used modulation frequency. It will be interesting to see if these peaks are reduced now that he has adjusted the modulation frequency to compensate.
The attached plot shows the full 2 FSR sweep from this afternoon, overlaid with the data taken in October and the output of a Finesse model. In general, in today's data we see larger contributions from the HGx0 modes than HG0x modes compared to the previous data. We suspect that is due to the razor dump mainly breaking the horizontal symmetry on the diode. Last time we used an iris, which may have been more even in blocking vertical and horizontal axes. We might wish to go back in and use a similar technique this time. Today's data also shows the much larger TEM00 peaks. Overall the SNR looks pretty good, and we'll move on to trying the automated sweeps from the control room.
The razor dump is still partially blocking REFL_AIR_B. We disconnected the EOM 45MHz input cable from the N.A. source, and reattached it to the 45MHz port on the RF distribution panel. We reconnected REFL_AIR_B cable to the demod board.
J. Kissel, R. Mittleman
Another day, another dollar's worth of ISI problems. This morning, I received reports of more than 0.1 [urad] RMS motion of the arm cavity BSC-ISIs -- now ISI-ETMX. As I've done every day this week, I'd resolved to just install improved QUAD damping filters with higher damping gain. However, the first step in this process is to use the current performance of the ISIs as input motion. As soon as I gathered the data, I found that the performance of the ETMX was polluted by a -- you guessed it -- ~0.5 [Hz] spike feature / oscillation / resonance in the X DOF (aligned with the SUS ETMX's L DOF), which rings up the 0.44 [Hz] and 0.56 [Hz] modes of the QUAD. The worst part about it is that this particular feature had appeared over-night.
Long story short, we did NOT find the source of the problem in the days worth of investigation, but it DID go away while we were investigating. Along the way, we've discovered several things that were poorly done on this chamber, which I'll detail below. However, now that feature is gone, I'll once again start the process of designing more beefy QUAD damping filters.
-------------
The Story, in brief (each bullet corresponds to the attachments, in order):
- Took performance spectra of X direction (ST1 T240s, ST2 GS13s, and QUAD Optical Lever Pitch), at 2014 Jan 30 15:00 UTC (before the morning meeting, local time). Found feature at 0.51 [Hz] (with a resolution 0.01 [Hz]).
- HEPI Isolated (Level 1 isolation filters, Position-Only Blends),
- ISI Isolated (Leel 1 isolation filters, ST1 XY T100mHz_N0.44Hz, all other DOFs, and ST 2 with 750mHz blends),
- QUAD Damped (Level 2.1 damping filters.)
- Looked at all Cartesian degrees of freedom on ST2 and ST1, only saw spike in X.
- Suspecting individual sensor flaws again, looked at raw T240 and raw CPS with only damping loops on. Saw nothing suspicious in any DOF.
- Closed loops again, tried blending ST1 without T240s (i.e. All DOFs on ST1 and ST2). Spike disappears, but the amplitude of the residual seismic noise is higher than peak amplitude of the feature. In-conclusive test.
- Suspecting loop instabilities, completely characterized X DOF isolation loop in both 750 mHz configuration and T100mHz_N0.44 configuration, measuring open loop gain transfer functions, closed loop gain transfer functions, plotting blend and isolation filters, etc. etc. While we found several problems, none of which would cause any instability.
- Remeasured performance of ETMX at 2014 Jan 30 21:00 UTC (during lunch / journal club local time), and feature disappeared. Good flippin' grief.
- Measured plant with isolation loops open to assess signs, appear to be self-consistent, though they don't match the conventions in T1000388.
The problems we found (which again, won't explain the ~0.5 [Hz] peak):
(1) Both sets of blend filters installed have flaws (see the first 2 pages of the "LoopChar" attachments):
- 750 mHz: The L4C Highpass has way too much gain at low-frequency. Now, as discussed earlier, the filter has to include the L4C response, but the roll-off of the complementary filter should start at a much higher frequency, say 200 mHz. Further, the displacement sensor low-pass should fall off (in frequency) faster than the L4C, they're currently both falling as 1/f (as indicated by the matching phase of -90 [deg]). I know these are supposed to be the "robust, OK performance" filters, but c'mon.
- T100mHz_N0.44Hz: The displacement sensor low-pass filter should fall off at-least faster than the L4C, if not faster than the T240. It current returns to flat in frequency, re-injecting displacement sensor noise above 100 [Hz].
(2) Though we measured matrix signs of the plant to be self-consistent (see 2014-01-30_1500_H1ISIETMX_Plant.pdf): at "DC," (the bottom of our band of interest)
- CPS = Flat in magnitude, and 0 [deg] phase, i.e. in phase, and in the same direction as the actuators
- T240 = Rising as f in magnitude +90 [deg], i.e. with the response to velocity flat above 4 [mHz]
- L4C = Rising as one factor of f in magnitude (+90 [deg] in phase) from being a velocity sensor, as well as two more factors of f (and another +180 [deg] in phase) from the inertial sensor response not yet compensated, for a grand total of what's shown: rising as f^3, with a phase of -90 [deg]
Comparing against the new document on conventions (T1000388), the individual elements are bonkers, and some coefficients are off by ~10-20%.
These ISIs really need some TLC.
All data posted in the above aLOG were taken with the following DTT sessions:
${SeiSVN}/seismic/BSC-ISI/H1/ETMX/Data/
2014-01-30_1817_H1ISIETMX_DampsOnly_RawCPS.xml % Calibrated spectra of raw input sensors for ST1.
2014-01-30_H1ISIETMX_SpikeStudy.xml % Performance ASDs of ST1 (T240s), ST2 (GS13s), and Test Mass (Optical Lever), calibrated.
2014-01-30_H1ISIETMX_ST1_X_WhiteNoise_ClosedLoop_OLGTF.xml % White Noise excitation, bandpassed between 0.1 and 10 [Hz], tuned to be driven closed loop
2014-01-30_H1ISIETMX_ST1_X_WhiteNoise_OpenLoop_OLGTF.xml % White Noise excitatino, bandpassed between 0.1 and 10 [Hz], tuned to be driven open loop
and all xmls and pdfs posted to this entry have been commited to the SeiSVN repository.
Aidan, Thomas, Eric G.
We installed the TCS HWS HAM4 optics this afternoon per D1201098. We've finished using that area and the chamber is covered again.
Full details tomorrow.
Here are the full details ...
We had to place ten optics/opto-mechanics assemblies. The D1201098 installation kit (cookie cuters) parts were placed to facilitate placement and alignment of optic assemblies. The assemblies were then bolted into position, summarized below:
Photos are attached below. Complete set is on ResourceSpace
We plan on installing the 4x 2" lens mounts and optics during the alignment of these optics or earlier.
Daniel noticed that following his inclusion of an ALS top_named part in the h1asc model this morning, the channels were being incorrectly named at H1:ASC-ALS_ instead of the expected H1:ALS-. Jim, Cyrus and myself spent some time diagnosing the problem and found that the problem is raised if the second part comes before the main part (ASC) in alphabetical order. In other words ALS was not correctly identified as a top_named part but ATT was. It appears the problem may be in the post_built python script where the "top_names" block property is parsed. We did some diagnostics with the h1asc model, so there may be some strange MEDM screens lying around. We never did a "make install" so the INI file was not changed since this morning. The investigation continues.
I did two make installs this morning, apologies if this caused probems.
following Rolf's suggestion we test the HWWD units with +-24V instead of +-18V, we first reproduced the start up error on unit2 in the DTS with 18V. In five power up cycles the unit did not auto startup, the LED is red and the reset button needed to be pressed to continue the startup. We then powered with 24V and found the same results, five start, none auto started. We then moved out 24V power supply to the CER and powered the unit attached to ITMY with 24V. Again we power cycled five times, once (20%) the system auto ran, four times (80%) it stuck at the red LED and needed a reset to continue. Results indicate error is not fixed with increasing the power from 18V to 24V. The DTS unit is left off, the CER unit was returned to 18V.
After adjusting F-Clamps with one requiring replacement due to a galling set screw, we locked up the HEPI. Following that all the Optical dummy masses were removed and bagged, now ready for HAM5. We finished about 1150pst. Thanks to the Apollo crew Mark & Scott.
I measured the MC cavity lock by adjusting the ifr frequency and measuring the transfer functions using an SR785. The source was injected into Exc A of MC common mode board and teed to ch1, meanwhile ch2 was connected to either IMON of REFL9 (1*FSR) and REFL45 (5*FSR). Data.txt is the data collected from REFL9 and Data_2.txt is that collected from REFL45. ArmCavityLength.m is the script that determines the length given the zero crossing of the projection. The attached plots show the results with a linear regression included.
The cavity length is determined to be
Implemented the new timing distribution system for the CPS's units (BSC's only) in the LVEA. Changes include using BSC2 CPS_1 unit as master. The timing signal is feed to a STS-2 Distribution chassis and distributed to all other CPS units. The STS-2 Distribution Chassis was placed in SUS-R6 floor rack.
Attached is a spectra of ITMX ST2 GS13 took after the timing system was changed (in blue), and compared with the reference from Seb's alog 9537 from last week (in yellow). Clearly, the combs do not appear any more.
Repeatedly in the past we had found the ISS PD's DC level jump to a state past 10Volts to somewhere arount 12V. The last time this occured last night (alog 9637). Staring at the PSL ODC screen, it told us that two things were wrong: BIT7 "ISS actuation saturation" and BIT11 "NPRO Relaxation Oscillation" were red.
Last night we fixed the ISS actuation saturation by readjusting the set point, but the PDs remaind in the odd 12V state.
Staring at the ODC screen this morning, BIT11 "NPRO Relaxation Oscillation" remained red. Taking that suggestion by ODC seriously, I went out to toggle the NPRO noise eater. Sure enough - the the ISS PD's switched back to the normal "<10V" state, and BIT11 went green.
Conclusions:
- Our long-standing ISS PD mystery is caused by noise eater oscillations.
- The PSL ODC system correctly announced this problem.
FYI, The ODC overview screen is available from the SYS tab on the site overview, and has links to all subsystem screens. The subsystem screens have a description string for each bit. Currently fully operational -including meaningful thresholds -are PSL, IMC, ISI and HPI for all currently commissioned systems, as well as SUS for MC1, MC2 and MC3. (All SUS's have a working ODC system installed, but the good settings are still a moving target due to commissioning.
I put the ODC master screen on video5. Due to the many not yet commissioned systems, there is still a lot of red there. In the attached plot, there is even more red due to the ongoing IMC length measurement. (stay tuned)
Related previous alogs:
I have been silently checking the signal chain of the REFLAIR and POPAIR RFPDs using the AM laser (a.k.a. PD calibrator) to make sure that they are functional expectedly.
Summary
The RF frequency of the AM modulation was adjusted in each measurement such that the demodulated IF signal was below 50 Hz.
Calibration of the amplitude modulation depth
We recalibrated the AM laser.
The current setting of the laser was changed recently because we opened up the current driver when we thought the laser diode had been dead in the early December. Then the laser head and its current driver were sent to Rich at Caltech for his extensive testing although the laser magically fixed itself and he didn't find anything wrong. So this was the first time for us to use the AM laser which had been fixed. Because of that mysterious event, I wanted to recalibrate the laser. First of all, Yuta and I measured the power to be 2 mW with an Ophir Vega without the attenuation filter. Then we measured the modulation depth for the amplitude modulation by using a Newfocus 1611 as a reference.
The new calibration for the amplitude modulation is:
P_am = 5.13 mW x (P_dc / 1 mW) * (1 V / V_drive)
where P_dc is the laser power at DC and V_drive is the drive voltage when it is driven by a 50 Ohm source. For example, if one puts this laser to a PD which then shows a DC laser power of say 2 mW, the AM coefficient is now 5.13 mW x ( 2 mW / 1 mW) /V_drive = 10.26 mW/V_drive.
REFLAIR_A_RF9 (S1203919)
Remarks:
The signal chain is OK. The PD response is smaller by 15% for some reason.
It seems as if the transimpedance is smaller by 15% than what had been measured at Caltech (LIGO-S1203919). The cable loss from the RFPD to the rack was measured to be 0.47 dB. Be aware that the demod gain is half of the quad I/Q demodulator because this is a dual channel demod (see E1100044). The demod conversion gain is assumed to be 10.9 according to LIGO-F1100004-v4.
REFLAIR_A_RF45 (S1203919)
Remarks:
The signal chain is healthy.
Found cable loss of about 1.5 dB. The measurements excellently agree with the loss-included expectation.
POPAIR_A_RF9 (S1300521)
Remarks:
The signal chain is healthy.
The measurement suggests that there is loss of 1 dB somewhere. I didn't measure the cable loss this time.
POPAIR_A_RF45 (S1300521)
Remarks:
The signal chain is OK. Though loss sounds a bit too high.
The measurement suggests a possible loss of 2.6 dB somewhere. I didn't measure the cable loss.
REFLAIR_B_RF27 (S1200234)
Remarks:
The signal gain is bigger than the expectation by a factor of 2.3.
REFLAIR_B_RF135 (S1200234)
Remarks:
The signal gain is bigger than the expectation by a factor of 1.5
POPAIR_B_RF18 (S1200236)
Remarks:
The signal gain is bigger than the expectation by a factor of 2.3
POPAIR_B_RF90 (S1200236)
Remarks:
The signal gain matches with the expected value, but I don't believe this.
There was a typo:
P_am = 5.13 mW x (P_dc / 1 mW) * (1 V / V_drive)
P_am = 5.13 mW x (P_dc / 1 mW) x (V_drive / 1 V)
For 27MHz and 136.5MHz, the RF gains are +19.8dB and +50.7dB, respectively. S1400079
The response of the BBPD isn't really flat over all frequencies. See D1002969.
The description in D1002969 is for the initial version. (The schematics seems up-to-date.)
The latest version has the rf performance as attached.
This is a follow up of the calibration measurements for REFLAIR_B and POPAIR_B.
I have updated the expected signal gain for these photo detector chains using more realistic gains which Koji gave (see his comments above). Now all the values make sense. Note I did not perform any new measurements.
In the following calculations, the quantity in red represent the updated parameters.
REFLAIR_B_RF27(S1200234)
Remarks:
The signal chain is healthy. There is loss of 0.92 dB somewhere.
REFLAIR_B_RF135(S1200234)
Remarks:
The signal chain is OK. There is loss of 3.9 dB somewhere.
POPAIR_B_RF18 (S1200236)
Remarks:
The signal chain is healthy. The signal was bigger by 9% than the expected.
POPAIR_B_RF90 (S1200236)
Remarks:
The signal chain is healthy. There is loss of 1.2 dB somewhere.
From these measurements, we can use POPAIR to infer the calibration for POP.
I looked at a recent lock acquisition while the interferometer was trying to engage the outer ISS loop. The LSC is relatively stable during this time, and the POP beam diverter is still open.
After undoing whitening gain and digital gain (2 ct/ct for POPAIR9/45, and 32 ct/ct for POP9/45), we find the following TFs:
This implies calibrations of 1.7×106 ct/W for POP9 and 1.8×106 ct/W for POP45.
There's a factor of 4 difference in power between POP and POPAIR (17 mW versus 68 mW with a PSL power of 23 W), so the values I gave above are off by a factor of 4. The demod gains should be 6.4×106 ct/W for POP9 and 7.2×106 ct/W for POP45.
I've attached a plot showing that the IMC has 'not been in a good state' (i.e. red) for the last 21 hours due to the ASC control switch not being on (summary bit 1). I can't see anything obvious in the alogs to determine why this is, anyone know? Thanks
The IMC WFS was off for approximately 8 hrs from Jan-30 01:50 to Jan-30 10:03 in UTC and it have been up in the rest of the time in the past two days. Probably it is because of the master gain which was lowered to 0.25 for some reason yesterday.
I've had a look at the last four hours and the IMC ODC is still red for the same reason (see first attached plot), but the PSL is looking green (2nd plot). I'm currently trying to make the PSL ODC plot for the last day but it's taking some time, so as soon as I have them I'll post it. But if this is to do with the NPRO relaxation oscillation (alog 9674) which Stefan reported turned the PSL ODC green it has not affected the IMC ODC.
Written by Yuta, posted by Koji, while he is waiting for renewal of his ligo.org account:
In the entry alog #9381, Sheila explained how the PDH signal is distorted by the broadened resonance
of the higher-order modes due to low finesse of the cavity.
Here in this entry I explain how the shape of the PDH signal can be modified by changing the sideband frequency.
[Motivation]
ETMX transission for green was larger than designed(designed:5% -> measured:36%) and cavity length lock does not stay long.
The PDH signal looks strange(see alog #9381). To explain the situation and see how we can improve the PDH signal,
we calculated PDH signal including HOMs.
[Method]
1. Calculate PDH signal including the effect of carrier HOMs and sideband HOMs.
2. Change sideband frequency to see how PDH signal changes.
The parameters I used are the same as the ones listed in alog #9381.
Calculated TMS is 5.076kHz and the sideband frequency before we have changed last night was 24.407079MHz.
HOM content and vertical scale are arbitary in the following plots.
[Result]
1. HOMPDH_sb24_4MHz.png and HOMPDHIQ_sb24_4MHz.png show the calculated transmission, PDH signals,
and XY plot of I-phase and Q-phase PDH signals, when the sideband frequency was set to the original value. This
IQ plot is very similar to what we have seen(see video in alog #9381) and agrees well with Sheila's calculation.
2. HOMPDH_sbonres+0_5TMS.png and HOMPDHIQ_sbonres+0_5TMS.png are the plots when one of the sideband
is at the middle of the TEM00 and TEM01/10 resonances. PDH signal gives zero crossing at TEM00 resonances,
but it also gives zero crossing at other HOMs. So, mode hopping rate is expected to be high.
3. HOMPDH_sbonres+TMS.png and HOMPDHIQ_sbonres+TMS.png are the plots when one of the sideband is
at the TEM10/01 resonance. PDH signal does not give zero crossing at TEM00 resonances, but if the correct offset
is given, mode hopping rate should be low. The IQ plot will be somewhat simple "8" shaped plot in this case.
See alog #9379 for what we have done using these results.
Written by Yuta
Calculation on demodulation phase dependence was done. See also alog #9429.
Requirement for the demodulation phase adjustment, TMS measurement and mirror alignment fluctuation to achieve frequency noise of few Hz are;
demod phase error < ~ 5deg
TMS measurement error < ~ 5% (~250 Hz)
mirror alignment fluctuation < ~0.3 urad
[Method]
1. Fix sideband frequency at the middle of the TEM00 and TEM01/10 resonances and calculate PDH slope and offset at 00 resonance for various demodulation phases.
2. Calculate PDH signal when the demodulation phase is set so that PDH offset will be zero at 00 resonance (see alog #9384).
3. Calculate zero crossing point of PDH signal dependence on differential cavity mirror misalignment (see alog #9429) when demodulation phase is off by 5 deg (see alog #9386) from the phase where the PDH offset is zero.
4. Repeat 3 by slightly changing the sideband frequency.
[Result]
1. misPDHdemod.png shows PDH slope and offset vs demod phase. Note that demodulation phase which maximizes the slope is different from the phase which minimizes the offset. The phase which minimizes the offset does not depend on TEM01/10 content, but the slope does.
2. misHOMPDH.png shows PDH signal when the demodulation phase is set so that PDH offset will be zero at 00 resonance.
3. zerocrossingPDH_5deg.png shows PDH zero crossing point shift by differential mirror misalignment when demodulation phase is off by 5 deg.
4. zerocrossingPDH_5deg_5percent.png shows PDH zero crossing point shift by differential mirror misalignment when demodulation phase is off by 5 deg and TMS measurement 5% wrong (worst combination).
[Discussion]
1. Assuming we can adjust the demodulation phase within ~5deg to minimize PDH offset by misalignment, measure TMS at <5% precision and alignment fluctuation is <~0.3 urad, misalingment induced frequency noise is smaller than few Hz.
2. The PDH signal looks nice when sideband is at the middle of the TEM00 and TEM01/10 resonances. It has about TMS of linear range and the range symmetric (compare with alog #9384).