Table work related to 70W install is still ongoing.
The ETMY M0 alignment sliders were changed on April 16, misaligning the optical levers. Jeff has returned the alignment sliders to their pre-April 16 value, re-centering the optical levers. Screenshots of optical lever and M0 opticalign trend for the last 10 days, and the current (good) slider values attached.
The access system at EX was taken down on Friday to allow APS contractor to continue with their work. The entry door to the change room is now unlocked.
Chandra, Dave:
while Chandra is working on CP4, and while MX-X1 cold cathode is trying to reacquire, I have bypassed these channels from sending cell phone texts (emails continue to be sent)
Bypass will expire:
Mon Apr 23 16:40:52 PDT 2018
For channel(s):
H0:VAC-MX_X1_PT343B_PRESS_TORR
H0:VAC-MY_CP4_TE253A_REGEN_TEMP_DEGC
we just lost H0:VAC-MX_X5_PT346B_PRESS_TORR, adding that to the list.
Jonathan, Dave:
Around 21:30 PDT last night (Sunday) h1boot froze up, presumably with the 208.5+day bug but the console message looks different. Every front end model eventually stopped processing. The front ends failed at various times, so some front ends showed IPC errors, others froze "green".
We reset h1boot via front panel reset-button. An FSCK file scan was enforced since the system had been running in excess of 232 days (boot servers can run far in excess of 208days before having a problem).
All frozen models came back with no restarts needed.
We are back to the weekend status of h1seib3 and h1susex computers are down due to 208.5+day bug.
CDS front end model status:
h1suspr2: awgtpman process has failed
h1susomc: DAC-KILL active (user watchdog?)
h1iopseiex: SWWD trip due to loss of h1iopsusex, DAC-KILLs active
h1susex: h1iopsusex, h1susetmx, h1sustmsx, h1susetmxpi: all down due to cpu lockup
h1seib3: h1iopseib3, h1isiitmx, h1hpiitmx: all down due to cpu lockup
h1pemmy: h1ioppemmy, h1pemmy: computer powered down for overtemp protection due to CP4 bake-out
I've restarted the awgtpman process for h1suspr2
I have verified that all the front end models continued to run overnight while h1boot was down, and their DAQ data was good. Only the EPICS channel access to the front end IOCs were unavailable. In the attached dataviewer minute trend plot for the past 24 hours, two LSC channels are shown; one comes directly from the front end over MX, the other is acquired via EPICS Channel Access using the EDCU. The EDCU signal is zero during the down time, the direct signal is unaffected.
The lasers are tripped off.
The PSL is not actually tripped off, because it is not yet connected to this interlock.
Appears to have tripped on Apr 21 2018 at 01:50:02 UTC. The ESTOP at the entrance to the VEA appears to have been engaged for a second or less. Glitch?
I've reset it.
Nutsinee, Sheila
Wensday afternoon Nutsinee and I went into HAM6 to tie up a few loose ends in HAM6 while we still had the interferometer beam available.
We had originally placed the beam dump to catch the IFO beam in reflection off of the beam diverter back side close to the diverter because we couldn't see the beam and were trying to dead reckon the position of the dump. With 3 Watts into the interferometer we were able to see the beam reflecting off the black glass, so Nutsinee and I slid it a few inches away. Attached photos show 1) where the interferometer beam hits the black glass side of the diverter (with the dump in its original close placement) 2) the final location of the diverter and dump 3) the beam hitting the beam dump is just barely visible in the lower right corner of the IR card.
We also checked the clearances of the single bounce beams on the other side of HAM6, which was just a double check of what Thomas logged here, and is pretty much in agreement with those measurements within the precision of the measurement technique.
Beam entering from HAM5 clears OM2 cage by 35mm, clears fast shutter wire without a problem, clears fast shutter structure by ~10mm. The beam from OM1 towards OM2 clears the AS_C lens by about 14mm, the edge of the OM3 cage by ~15 mm, and when the shutter is closed it is directed into the pipe beam dump. The beam from OM2 towards OM3 clears the OMC shroud by about 17 mm.
Georgia, Robert
This entry gives results from the test discussed by Georgia here: https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=41559
Sometimes during PEM injections, we sanity check that external electric fields (like from a lightning strike) do not significantly affect DARM by sneaking into the chamber through a viewport. A repeat of these injections allowed for a comparison of the field measured by the EFM to the test mass motion that has been induced in the past by similar injections. In the past, we only did a single frequency in the bucket - because the integration time to see the signal in DARM was long.
We repeated the injection by placing an insulated plate over the illuminator port of the EX chamber, and driving at 211 Hz with a voltage of about +/- 11 V relative to the chamber. Similar injections have produced an rms DARM signal as high as 1.5e-21 m in the past, though this is variable, and sometimes we can’t integrate long enough to see the injection in DARM.
The figure shows an EFM spectrum for this injection and DARM for a similar injection in the past. The calibration from the log referenced above gives an rms field at 211 Hz of about 1e-5 V/m at the EFM. Assuming similar conditions to those in the past, we get a coupling of about 1.6e-16 meters of DARM motion per V/m measured by the EFM, for this injection configuration. The SNR of the EFM signal for the injection appeared to be nearly ten times greater than the DARM SNR had been during similar injections in the past. Shielding may differ for different injection points, but at least for this port injection, the EFM appears to be more sensitive than DARM.
I calibrated our EFM spectrum into DARM, this time using Robert and Georgia's electric field to meter TF numberI assumed that
due to the test mass suspensions, where
is some constant. From Robert's measurement I found
. Then, calibrating EFM voltage output noise
into displacement noise:
where
from alog 41591, and
. The estimated displacement noise is plotted below. Think of this as an upper bound for the ambient electric field noise, since we are not sure our EFM noise floor below 100 Hz is not sensor noise, and this is literally a single point measurement of
.
Sheila, Dan, Alexei, Nutsinee, TVo
This is the analysis of OMC mode scan data taken on Thursday. The data is a bit noisy even though we turned down the purge air and had all the suspensions (including the VOPO) and ISI damping. The AS Centering loops were turned on and the OMC_ASC was also turned on which helped to reduce the TEM01 contribution. It's not very easy to tell what the actual peaks of the modes are so I applied a 500 Hz low-pass filter to the data to try to resolve an average peak intensity in OMC_DCPD_SUM:
Estimated Results:
Lens2 closest to the OPO: 88%
Lens2 in center Position: 86.7%
Lens2 furthest from OPO: 83.3%
These seem consistant with our Finesse mode matching model.
Note: We took data for about a minute but I focused only on one set of peaks that I knew were the 02 and 00 modes.
ETMX:
System continues to be protected by the Hardware Watchdog. h1susex models are not functioning, DAC outputs for SUS-ETMX and SUS-TMSX presumably frozen at last value. Because the IPC to h1seiex is frozen, the Software Watchdog on h1seiex has tripped and all DAC drives are zero for ISI-ETMX and HPI-ETMX.
Possible Sunday recovery is to reset h1susex, which may dolphin glitch h1seiex and h1iscex. This is not an issue since h1seiex has SWWD tripped and is therefore not driving.
ITMX:
System continues to be protected by the Hardware Watchdog. h1seib2 models are not functioning, DAC outputs for ISI-ITMX and HPI-ITMX presumably frozen at last value.
Possible Sunday recovery: there are no IPC errors in the corner station resulting from the loss of h1seib2. One minimal-impact recovery would be to power off h1seib3 and remove its Dolphin cable before powering it back on with a modified h1iopseib3 model which temporarily disables the SWWD. This would restore SEI-ITMX function and not precipitate a restart of most of the corner station models.
Monday Recovery: reset frozen systems, restart any subsequently glitched models, rebooting all computers with uptime exceeding 208.5 days. A slower recovery will be to upgrade RCG to 3.4.2 (restart all models).
After making it through the week with no critical systems freezing up, two systems froze overnight: h1seib3 (ITMX) and h1susex.
If these systems are needed today please call me and we can coordinate a reset. Otherwise we will reset most machines tomorrow.
I'll be mostly at Y-mid tinkering with the GN2 flow through CP4. Chandra R. is my "phone buddy" and I'll make a comment to this entry when I leave.
As found, GN2 flow through CP4's regeneration circuit was steady and indicated on the first scale graduation (12 SCFH x 100). The dewar head pressure(s) were 10 psi and 12 psi as per the mechanical gauges -> I opened the Pressure Build valve 1 turn ccw and the dewar head pressure increased by 2 psi over 20 minutes. Correspondingly, the GN2 regeneration flow increased to a varying 40 - 50 SCFH x 100. I did not notice any reverse flow through the Fill Connection line. The Regeneration Temperature decreased, as expected, with the increase in flow. Even so, I don't feel comfortable leaving the site with the Pressure Build valve open as we have no way to remotely monitor the exhaust line pressure and I can't be sure that the dewar head pressure has stabilized. As a compromise, I closed the Pressure Build valve and, instead, adjusted the dewar head pressure (a.k.a. vapor pressure) regulator (a.k.a. "economizer") 1/4 turn cw. This should slowly increase the dewar head pressure a little over the next day or so and the regeneration flow should also increase a little as a result.
1040 hrs. local - > Leaving site now via one last check at Y-mid
Calibration of the field meter does not need knowledge of the input capacitance. With the calibration plates, the electic field on the sense plate is simply E(cal)= V(cal)/d where d is the calibration-sense plate separation. If you want to improve the accuracy you will need to account for the thickness of the copper disk on the sense plate and a few percent error due to the fringing field. The current sensitivity curves are pretty close to the ones measured in the prototype. How did you handle the factor of 2 due to the two plates on each coordinate and the output which is the difference?
We were a little confused about how to calibrate the EFM. It's not such an easy problem as it first seems.Calibration Plate Voltage to Electric Field TF
V_cal refers to the potential difference between the calibration plate and ground. Ground is connected to the body of the EFM. The sensor plate is kept isolated and should be at voltage V_sense = V_cal * d2/(d1 + d2) where d1 is the distance between the cal plate and sensor plate, and d2 is the distance between the sensor plate and the body. If we assume that the electric field E_cal is constant over the entire EFM, then I think we ought to be using the total distance d = d1 + d2 between the calibration plate and body for E_cal = V_cal/d. d1 = 1/2 inch = 1.27 cm, and d2 = 5/8 inch = 1.59 cm, so d ~ 2.86 cm and E_cal/V_cal = 1/d ~ 35.0 (V/m)/V using this method. However, we became concerned about the geometry of the EFM affecting this result. There is a copper disk which connects the sensor plate to the sensor pin, and there are a bunch of large screws between the sensor plate and the body. We decided to compute an "effective distance" using the capacitances we measured between the cal and sense plates (~11pF), and the sense plate and the body (~19pF) via E = Q/(2 A e0), where A is the area of the plates (~0.01 m^2), e0 is the vacuum permittivity, and Q is the charge on the cal plate. Q = C V, so we can recover E/V = C/(2 A e0) = 1/d, so our effective distance d = (2 A e0)/C, where C is the total capacitance between the cal plate and the body (~7pF). Using this method, E/V ~ 38.9 (V/m)/V, not much different than our result from 1/d. This is the number we used to calibrate from V_cal to E_cal. I don't know what value was used for the initial prototype.Differential Amplifier Factor of Two
We did not account for this. We did not understand that the EFM body was grounded, so that the body absorbs the E_cal field by inducing charge on its near face. In the presence of a large external electric field both sense plates will have voltage induced, so we will get twice the response from the EFM differential amplifier circuit. We measured a TF from V_cal to V_out where V_out is the voltage output of the EFM differential amplifier circuit, and got V_out/V_cal ~ 0.8 from 5 kHz down. This should be multiplied by 2 for the V_out/V_external TF.Corrected Plots
Plot 1 is the newly calibrated ambient electric field ASDs recorded by the EFM. Plot 2 is the V_out/V_cal TF.
We (the EFM calibration team) never understood that the sensor plates are virtually grounded by the op-amp inside the EFM until we saw Figure 2 of T1700103. This is why we kept insisting that E = Vcal/d should use d = distance between calibration plate and the EFM body: we thought that the sensor plate was an floating conductor. I fixed our calibration to account for the grounded sensor plates. If I use E = Vcal / d where d is the distance between the cal and sensor plates (d ~ 1/2 inch ~ 1.27 cm), I get. If I account for the copper plate and fringing fields by using our measured capacitance between the calibration plate and sensor plate (C ~ 14.7 pF), I get
(Area A of the plates is ~ 0.01 m^2). This is the E/V calibration I used for the plots below. Also included was our cal volts to EFM output volts measured calibration value of 0.8 V/V. This was multiplied by two to account for the differential response of the EFM to external electric fields, and inverted to give
. Unfortunately, with this corrected calibration our prototype EFM spectrum is worse than we originally thought. In fact, it's worse than your final prototype spectrum from T1700569 by about a factor of two. I am not sure why this should be the case. Rich's LT Spice model has a output voltage noise floor of about 200 nV/rtHz at 200 Hz upward. In your Figure 2 of T1700569, you report a Vn of 110 nV/rtHz, so maybe this result is correct.
The calibration is simpler than you make it. With the cube grounded and the calibration plates mounted on the sense plate, the electric field induced on the sense plate is E = V(cal)/d (with small correction for fringing and the copper plug). If you want to make a model for the calibration to predict the sensitivity that is more complicated and requires knowledge of the capacitances and the potentials between the sense plate and the cube.
Craig, you refer to T1700103 figure 2 to understand the virtual ground. This is not the correct schematic for the implementation of the EFM that was recently built. Each EFM input is simply 10^12 ohms to ground (in parallel with the sense plate capacitance). There is no virtual ground provided actively by the operational amplifier.
Final note on the EFM calibration. Conclusions:After a discussion with Rai and Rich we determined the correct calibration is
where
is the driven voltage on the cal plate,
is the induced voltage on the sense plate, and
is the distance between cal and sense plate. We need to know the voltage induced on the sense plate. To do this I simulated the circuit in the first picture. Again, we measured the capacitance between the cal and sense plate to be 14.7 pF, while the capacitance between the sense and body was 19 pF. I found
above 10 mHz. Solving for
gives the result above. The final plot is the correctly calibrated ambient electric field spectrum.
I am very sorry for having generated all this confusion. The sense plate is not a virtual ground, that was the case in earlier circuits. In this
circuit the proper formulation for the electric field on the sense plate from the calibration plate is
V(cal) - V(sp) V(cal) C(cal-sp)
E(cal) = ---------------- = ---------------------------------- So, the calibration field is smaller than in the case for the sense plate held
d(cal-sp) d(cal-sp)(C(cal-sp)+C(sp-allelse))
at ground potential which makes the field meter more sensitive. Which is what you found. The error is purely mine and not Rich Abbott's or any
of the people in the electronics group. It comes from my not thinking about the calibration again after the circuit was changed from one type
to another in my lab.