[Peter, Koji]
Follow up entry for ALOG LHO 41420
Optical Transmissivity of the EOM
The optical power was measured before and after the EOM. Because of the space constraint, the "BEFORE" and "AFTER" measurements had an HR mirror and a 2" lens between the power meter and the EOM, respectively.
OLD EOM: T_EOM = 175.0mW/177.8mW = 0.98 +/-0.01
NEW EOM: T_EOM = 178.3mW/180.0mW = 0.99 +/-0.01
We did not find any significant change of the transmission performance for the new eom.
Modulation depth
The modulation depth of 9.1MHz and 45.5MHz modulations were measured with an OSA. The other two modulations were too small to measure. The OSA output was captured with a digital oscilloscope with one channel adjusted for the carrier peak and the other for the sideband peaks. The offsets (PD dark, Vofs between the channels) were subtracted in the analysis. 10 scans were taken for each case, meaning N=20 samples for one modulation with upper and lower sidebands combined. Driving RF power for each case is described in the following section.
OLD EOM 9.1MHz: m = 0.187 +/- 0.001 [rad] (N=20)
OLD EOM 45.5MHz: m = 0.287 +/- 0.001 [rad] (N=20)
NEW EOM 9.1MHz: m = 0.210 +/- 0.006 [rad] (N=20)
NEW EOM 45.5MHz: m = 0.197 +/- 0.007 [rad] (N=20)
The modulation for 9.1MHz was adjusted to have approximately the same number as before.
The modulation for 45.5MHz got maxed out with the driver capability together with the additional loss at the power combiner (see below)
Driving power
The RF driving power levels for the above modulation depths were measured. The RF signals at 24.1MHz and 45.5MHz are combined with a power combiner (RF-Lambda / RFLT2W0002GN).
OLD EOM 9.1MHz: EPICS setting 16.8dBm / Delivered RF 16.68dBm
OLD EOM 45.5MHz: EPICS setting 23.4dBm / Delivered RF 23.36dBm
NEW EOM 9.1MHz: EPICS setting 23.6dBm / Delivered RF 23.56dBm => Estimated modulation 0.191 rad
NEW EOM 118.3MHz:Delivered RF 9.84dBm => Estimated modulation 11.7 mrad
NEW EOM 24.1MHz: The cable in the PSL 14.12dBm -> (ATTN at the amp input: 5dB) -> Amplifier output 28.98dBm
-> Power Combiner output (Derivered RF to the EOM) 24.6dBm => Estimated modulation 12.7 mrad
NEW EOM 45.5MHz: EPICS setting 27.0dBm (maximum setting) -> Driver output 27.3dBm -> Power Combiner output (Delivered RF to the EOM) 23.76dBm
=> Estimated modulation 0.210 rad
Note1: Daniel mentioned that the amp gain was supposed to be 16dB. However, the gain of ~20dB was observed.
Please check if this is OK. Is the output too big for the amplifier used?
Note2: The power combiner is causing the estimated loss of 4.4dB and 3.5dB for 24.1MHz and 45.5MHz respectively.
Attachment 1: Installed EOM
Attachment 2: Driver arrangement beneath the PSL optical table.
Attachment 3: Power splitter isolation (I didn't like that the power splitter connectors touching the amplifier chassis, which may cause some glitches.)
Attachment 4/5: Old EOM Input/Output surface (Microscope view, a few particulates visible, but the surfaces aregenerally in a good condition.)
Attachment 6: Mod. depth meas, an example scope screenshot.
Why is the power combiner not screwed to the output of the 45MHz amp?
Sheila, Jeff K, Hugh, Jamie, Sheila
We did some investigating of why the signs were flipped on the AS centering loops, which was made more difficult by some SDF confusion.
Sign flip
The reason why the sign was flipped for the AS centering loops was explained in 40853, Jeff corrected an error in the sign convention for the tip tilts. This means that the signs will also be wrong for the refl centering loops and the OMC ASC loop that feedsback to OM3. This probably also explains part of the difficulties that T Vo had in closing the OMC ASC loops.
I've flipped the sign of all REFL and AS centering loops, and flipped the sign of the OM3 actuation for the OMC ASC by changing the sign in the output matrix (DOF2TT). I accepted these in SAFE.snap and observe.snap
SDF confusion
Last night when Terry and I realized that we could only close the AS centering loops by flipping the sign, we looked at the SDF file for the OMs (which are on the SUSOMC model). We saw that in the observe file (which is the same as the safe file) all the outputs were turned off, which doesn't make sense. This led to not trusting SDF. Jeff went back through the autoburt snapshots and realized that some wrong settings were stored in SDF when the OMs were moved to the OMC model (38827).
Currently when new channels are added to a model, they are not monitored in SDF. It would be better if the default were to monitor new channels.
[Aaron Viets, Alex Urban]
I modified the filter generation code to store a transfer function for the pcal correction factor. The name of the numpy array is "y_arm_pcal_corr." It is an array with 3 rows, the first of which is frequency (0 to 8192 Hz in increments of 0.25 Hz), and the next two of which are the real and imaginary parts of the transfer function at that frequency. So, for example, to get the pcal correction factor at 100 Hz, you would do:
filters['y_arm_pcal_corr'][1][400] + 1j * filters['y_arm_pcal_corr'][2][400]
Unfortunately, we don't know a way to store complex values in the filters files, so this is haw we have to store them (for now, at least).
I made two filters files for LHO, one for GDS and one for DCS. They are in the calibration SVN under aligocalibration/trunk/Runs/O2/GDSFilters/ and the names are:
They are valid for the last portion of O2, the same time periods for which the latest filters were used as listed on the O2 calibration configurations wiki.
I did a quick spot check to see that the transfer functions were computed correctly, by just comparing their values at the calibration lines to the values included in the filters for those lines, which we know to be correct.
Sheila, Craig Since Koji and Peter have replaced the PSL EOM, the phase of IMC PDH error signal is altered. Shelia and I went out to the PSL racks and looked at the I and Q demodulated IMC error signal. To get the carrier PDH slope to be along I, we adjusted the error signal delay from 6.4375 ns to 13.4375 ns. You can see the rotation of the IMC PDH error signal in plots 1 and 3, which are pictures of the I and Q demodulated error signal in an XY oscope plot.
21:31 UTC Sheila to HAM6 Sheila back 22:06 UTC Aidan to LVEA Aidan back 22:26 UTC Cheryl to PSL enclosure 22:28 UTC Gerardo to LVEA to take picture of spool piece 22:44 UTC Gerardo back 22:57 UTC Georgia back from squeezer bay
Adjust the mirror mount before the rotation stage and the one at the base of the IO periscope to partially bring the beam back to the input modecleaner. One can certainly see flashes as MC2 swings. The knobs were moved less than 1/16 of a turn in both axes. I limited the power to the input modecleaner to 5 W by using the half waveplate and polariser combination at the output of the pre-modecleaner. The output of the photodetector on the table that monitors the power going into HAM1 did not change appreciably from ~60 mV. Since the new EOM is not resonant at 24.1 MHz and because of some changes to the RF signals, the phase and sign of the error for the input modecleaner may need some adjustment.
Calum, Craig, Luis, Georgia, Peter, Travis, Betsy, Filiberto, Ed, Richard, Rich We had a hard time tracking down the source of an open circuit in a single wire(Y-axis, negative leg of the differential signal sent from the electrometer out from the vacuum system) of the electrometer cabling. We spent much time taking every section of the cabling apart (air and vacuum) only to find that we couldn't see any problem. We are absolutely certain that this pin was not functional at the start of our hunt, but somewhere in the process it fixed itself. Very disturbing. We were able to verify the performance of all aspects of the design, but as we hoped, we now have a list of tweaks that we will apply to the electrometer back at CIT. A timeseries of the differential signals coming out of the EFM revealed the background noise in the chamber to be of order 50mV pk-pk. We were able to easily see people moving around in the chamber, and were able to see the door cover being flapped around by Georgia (when we asked her to flap it). 1. We feel the gain in the EFM should be increased by up to a factor of 100. We will add a bit of gain inside the EFM, then add more gain to the in-air part of the system. This is to ensure the background field noise is above the ADC input noise (whitening). 2. We will improve the mechanical mounting of the calibration plates such that it is easier to shift them from one axis to another 3. We will improve the robustness of the serial communications link used to adjust the common-mode rejection ratio (CMRR) as this proved problematic. 4. We want to limit the high frequency bandwidth of the EFM. 5. We want to investigate a 1.7MHz oscillation seen when the field meter was swung causing an electrical saturation. It appears to be phase reversal on one of the amplifiers. This went away upon power cycling. We verified that the CMRR can be adjusted in situ to better than -60dB. We also concluded that this adjustment should be done in-chamber as the bench results taken in the optics lab were different than the results obtained in the installed environment. We verified the 'dark' noise of the EFM to be approximately 200nV/rtHz at 100Hz, which is consistent with design We measured the background differential noise in X and Y to be approximately 5uV/rtHz at 100Hz as measured at the differential output at the rack (plots to follow). I believe the calibration of this device to be approximately 64mV per volts per meter at 100s of Hz or so, although this needs to be further investigated (I get this from 16mv/v/m times 2 for differential sensitivity, times 2 for the differential driver gain). As Rai cautioned us, we need to be careful with the plate spacing distance due to irregular features between the plates (copper buttons), but a simplifying view is given by the capacitances between the calibration plate - sense plate - and ground of the EFM body. The observed ambient spectrum seemed a bit devoid of features to me and was approximately a factor of 10 lower than the field observed in the optics lab.
Attaching a picture of the EFM suspended in chamber next to ETMX, note that the viton damping was not yet installed, and the ISI was locked for all measurements we did.
In this picture the sensor plates are grounded.
Craig, Georgia Here are some initial spectra and transfer function we took of the Electric Field Meter (EFM) in the X-end chamber. More thorough analysis/noisebudgeting will be done by Craig and Georgia on Monday. Plot 1 is Georgia's plot of the optics lab ambient electric field spectra vs. our in chamber ambient electric field spectrum in cyan. If this result is to be trusted, we see a significant reduction in electric field noise in chamber vs in the optics lab. Plot 2 is the EFM positive Y calibration from driven volts on the EFM calibration plates to differential output volts as detected by the sensor plates. This means that the calibration plate nearest to the positive Y electric field sensor plate was driven by the SR785 using a 1 V oscillation, and the EFM differential Y output response was measured. Plot 3 is the ambient electric field in the X-end chamber according to the EFM Y direction. Plot 4 is the Y common mode rejection. To take this measurement, both calibration plates on the positive and negative Y ends of the EFM were driven with the same 1 V oscillation. The EFM Y output was then minimized using a digital potentiometer to balance the response. More measurements we want on Monday: 1) Negative Y Calibration TF 2) Grounded Y Spectrum 3) Noise Floor 4) ISI Driven Ambient Electric Field Spectrum 5) Retake the above measurements
The following in vacuum cabling was added to ETMx for the Electric Field Meter (EFM). While the EFM is not the final version the cabling installed is the final version.
We added LIGO-D1800089-v2 SN S1800629 and LIGO-D1800090-v1 SN S1800631.
With reference to page 11 of the LHO ETMx in vacuum cable routing drawing, LIGO-D1300007-v2 , these above additions were placed in the existing ISC-QPD (532 NM) path.
It should be noted that a 15-pin cable bracket, LIGO-D1800072-v1 was also added between the 15 pin sections. However, the wrong base was sourced for the required cable bracket, LIGO-D1001347-v3, between the new LIGO-D1800090-v1 and the existing D1000924. So this is pending. Either a new based has to be sourced or 3 cable portion replaces the existing 2 cable portion of D1001347 on the table.
We will update the required SYS drawings to match this (and ICS).
Added 150ml cooling water to PSL Crystal chiller. Diode chiller water level is good. No change to both filters.
Aligned beam onto the PDB photodetector in the ISS PD box. Also realigned the beam onto the quadrant photodiode. The effect of which can be seen in the attached plot. Engaged the first loop power stabilisation this morning without much hassle. The calculated diffracted power percentage is off as the coefficients need to be calculated. Without doing some loop measurements, the gain slider setting of 18 dB maybe the wrong value.
Old coefficients for calculating the diffracted power percentage are displayed in OriginalCoeffs.png. The new coefficients are displayed in NewCoeffs.png. With the reduced diffracted power, I changed the limits of the plot in the ISS MEDM screen from 20 to 5.
Due to hardware BIO logic change in the ISS 2nd loop board (D1600298, HIGH/LOW=NO/NC in V2, HIGH/LOW=NC/NO in V3), I removed or added NOT in all relevant BIO control and readback channels in psliss frontend.
I removed H1:PSL-ISS_SECONDLOOP_REFERENCE_VALUE_CAL filter and H1:PSL-ISS_SECONDLOOP_REFERENCE_VALUE EPICS channel, these were necessary before as the slow offset loop and digital excitation combined had one dedicated analog input, now these are added together with the 3rd loop. This analog input was reassigned to the BNC input on the chassis.
I just saved the model but hasn't compiled yet.
Right now it seems like BIO is not working. Despite the logic change the old model should be working (with inverted logic), but flipping BIO control channels (e.g. H1:PSL-ISS_SECONDLOOP_PD_SELECT) doesn't seem to change BIO readback (e.g. H1:PSL-ISS_SECONDLOOP_PD_SELECT_MON). Is the board connected at all?
I went to the rack and confirmed that the chassis was not powered on. I'll wait until people are done with any work needing PSL light.
Compiled. Not installing for now as this will interfere with PSL work. In the mean time I made a new MEDM screen for the second loop (1st screen shot).
Also attached are before/after screenshot of the BIO and slow offset path.
We're reviewing the HWS SLED situation. We have only one spare for the ITMX SLED and no spares for the ITMY SLED.
We're averaging about one SLED every 8 months during intensive usage.
In storage cabinets next to BSC3.
At the request of the controls engineer, the Yend HEPI platform was unlocked. No issues other than the usual terrible access in unlocking.
Ran Cartesian Range-of-Motion tests of 0.5mm for DOFs X Y Z RX RY & RZ. Probably sufficient to do X Y & Z but forgot about that before getting started.
The attached plot shows the X Y Z Range of Motion with the local sensors over laying one another. This shows no bad actors of local sensor clipping, slope differences or changes. HEPI is clear to +- 0.5mm. Will check larger ranges most importantly for Y (tidal) another time but this will get us by for now.
The HEPI and ISI platforms are Isolated.
The hints of clipping seen in the above plot was bothering me so I ran another stroke this morning, this time to +- 0.75mm on X Y & Z dofs. I ran the offsets with the platform Isolated this time.
The attached shows, again, no evidence of any clipping on the platform. Again, any problems would apprea as clipping or slope changes.
The TCS chiller pump has been rebuilt and should be ready to act as a back-up now. In the future if the water pump needs to be rebuilt it uses a a type 21 shaft seal, 5/8" shaft size, 1 1/4" seat bore. The replacement o-rings are 4x dash number 012 and 1x dash number 242. It also uses a standard external retaining ring with a 5/8" OD. Use a light grease to seat the shaft seal, or else the rubber will tear (voice of experience here, oops).
The chiller is currently running in a small closed loop to see if any leaks develop overnight, it is on the mezzanine with its other siblings.
The rebuild survived a week of recirculating, so it is now drained and sitting at standby waiting for the day it is needed again.