This is a low level sanity check and a part of the recent delay study (e.g. 29259). I have measured a transfer function between DARM2_OUT and SUS-ETMY_L3_ISCINF_IN1 using dtt while the interferometer was locked last night. The measurement agrees with 1 cycle user model delay (=61 usec). See the attached.
Here is another low level sanity check. The attached shows a tranfer function of signals from the SUSETMY user model to its associated IOP model. It shows a 1 user model clock delay (61 usec) as expected. There is a large deviation above 7 kHz which I don't know why. The FIR filter (T1600454) was included in my 'expected' model.
WP6220 Inclusion of DBB channels to DAQ to monitor jitter of HPO
Daniel, Dave:
a new h1psldbb model was installed and the DAQ was restarted this afternoon (14:50 PDT). Daniel decided that this version initially write its fast channels to the commissioning frame only while the ECR for science frame inclusion was being processed. Daniel's ECR (E1600301, FRS6386) has been approved and these channels will go into the science frame on the next DAQ restart.
Krishna had noted in a log in the secret SEI logbook that the endstation BSC tilt subtracted sensor correction wasn't performing as well as the corner station sensor correction. This seems to have been due to a high pass added to the tilt subtracted seismometer path. This filter is supposed to help suppress signal from the BRS 8mhz resonance, but it seems to have been distorting the phase of the STS signal too much at 100mhz. The first attached plot is of an older (I think) high pass in red and the "problematic" high pass in blue. I've switched ETMX to the "old" high pass, second plot are the ground STS to St1 T240 tf for each endstation. Red trace is EX, blue is EY. It's subtle, but EX is doing better in the 100-200mhz band, if you squint. I'm going to leave the endstations in this configuration overnight, while people in the seismic group can come up with reasons why this is a bad idea.
Jenne, Evan
We looked again at RFAM on the 9 MHz REFL readout.
The attachment shows REFL9I (and REFL LF) for four different PD powers. Additionally, at the fourth power we locked the ISS outer loop (dc coupled with boosts) just to check that the RFAM does not change. The REFL centering loops were on the whole time.
At no power were we able to see anything that looked shot-noise limited, so we were not able to independently check the transimpedance and demod gain for REFL9I. However, the limit placed by the high-frequency noise already seems to indicate that we are missing some gain in the signal chain. Thus far I have been using 2900 V/W for the PD transimpedance plus demod TF, but this would produce spectra that are below the expected shot noise level.
I double-checked the schematics for the REFL LF path and found that the current digital calbration from counts back into watts seems OK. The PD powers given in the attachment are based on this LF calibration.
Finally, note that the dark noise at several kilohertz is larger than the noise when the PD has power on it. No clue about why.
The attachment shows REFL9 and REFL45 signals (in ct/rtHz), with the colors corresponding to the powers given in the previous attachment.
REFL9Q appears to be shot noise limited above 100 Hz, since the noise grows with the square root of the power.
In comparison, REFL9I looks fishy. Its dark noise is higher than REFL9Q, and above 500 Hz shows a noise that is lower than the REFL9Q shot noise.
We are tempted to say that the analog Q channel of the REFL 9 demod board is broken (recall that analog Q corresponds to digital I, and vice versa), or the corresponding whitening channel is broken. (However, since analog Q is teed off and hooked up to the summing node board, it's possible that there's some strange interaction with the SNB.)
Anyway, if we use REFL9Q to calibrate the rf gain of REFL9, this implies a total gain of 2.88e6 ct/W (= 4.4e-4 ct/rtHz / sqrt(4*h*nu*P0), with P0 = 29 mW). We can refer this back to the demod board output by undoing the digital gains (0.18 ct/ct), the ADC conversion (2^16 ct / 40 V), and the whitening gain (12 dB) to arrive at an rf gain of 2600 V/W, which is not too far off from the old value of 2900 V/W.
FAMIS#6491
No water was added to the crystal chiller, the water level was at the Max line. The diode chiller did not have a low water level alarm, so I also did not add any water.
Title: 10/06/2016, Day Shift 15:00 – 23:00 (08:00 - 16:00) All times in UTC (PT) State of H1: IFO lost lock due to PI ring up. IFO was coming back up when I came in. Was able to damp PIs M2 and M10. IFO relocked at NOMINAL_LOW_NOISE with no problems Outgoing Operator: N/A Activity Log: All Times in UTC (PT) 14:20 (07:30) Chris & Apollo – Going down Y-Arm to work on beam tube sealing near CS 14:30 (07:30) Damped PI modes M2 & M10 – IFO relocked at NOMINAL_LOW_NOISE 14:50 (07:50) Robert – In LEA doing injections 15:10 (08:10) Peter – Going into PSL to adjust power & install new PD (WP #6219) 15:10 (08:10) Christina – Forklift crate from LSB to Mechanical building 15:12 (08:12) Richard – In MSR to replace batteries (WP #6218) 15:15 (08:15) Karen – Cleaning in Optics Lab 16:00 (09:00) Kiwamu – Going into PSL for PD install (WP #6219) 16:09 (09:09) Karen Out of Optics Lab 16:20 (09:20) Peter & Kiwamu – Out of PSL 17:32 (10:32) Robert – Running injection 21:45 (14:45) Dave – Adding new DBB signals to frames & DAQ restart (WP #6220) Shift Details: 10/06/2016, Day Shift 15:00 – 23:00 (08:00 –16:00) All times in UTC (PT) Support: Cheryl, Incoming Operator: Travis Shift Summary: Broke lock around 14:00 (07:00) due to PI ring up. At around 14:30, damped PI Mode #2 by changing phase from 30 to 80 and PI Mode #10 by changing phase from 30 to 80. Modes responded quickly and we relocked at NOMINAL_LOW_NOISE with no problems. PI Modes 2 & 10 rang up again – damped mode 2 buy changing phase from 80 to 30. Damped Mode 10 by changing phase from 80 to 60. Most of shift spent in commissioning and relocking.
Following up on entry 30273, I computed the coherence and transfer function between ISS_PDA_REL_OUT (which should be calibrated in RIN units) and CAL-DELTAL_EXTERNAL (including the proper calibration). Coherence is good enough to estimate a transfer function over all the frequencies above 10 Hz. I'm not injecting any additional noise, just using the signals as they are, so the fact that we have coherence doesn't necessarily mean that we really have a coupling of intensity noise to DARM.
However, the transfer function has a very interesting shape (see figure). It's behaving like 1/f^3 up to ~80 Hz, and above that frequency it increases like f. The region below 80 Hz might very well be consistent with radiation pressure coupling of intensaity noise. We'll have to run some numbers to be sure that this makes sense. I have no clear explanation of the increase above 80 Hz.
Addition:
A quick and dirty estimate of the expected coupling of RIN at the ISS PDs to DARM due to radiation pressure
x = 2 deltaP / c / (m * (2*pi*fr)^2) / (fr / fr_pole_doublecav) = 2 P_arm / c / (m * (2*pi*fr)^2) / (fr / fr_pole_doublecav) * RIN
At 30 Hz the coupling should be about 2e-11 (maybe off by a factor of 2 or so due to the two arms, etc..). This is many orders of magnitude LARGER than what measured in the TF discussed above. So it is unlikely that PDA/PDB see real intensity noise that goes into the IFO.
I checked how stable this transfer function was over time. I picked the lock stretch that started around GPS 1159781417, last night.
The first plot shows the transfer functions CAL_DELTAL / PDA_RIN for 23 segments, each 600 seconds long. The second plot shows the same transfer functions, but divided by the overall mean, to emphasize the variations. It's clear that there are variations up to ~40% during this time period.
FInally, the last plot shows the value of the transfer functions averaged in four different frequency bands, as a function of time. This shows more clearly the variation and the more accentuated trend at the beginning of the lock stretch.
I ran a BruCo scan for the last night lock, using ten minutes of data when the range was at ~65 MPc. Results are available here:
https://ldas-jobs.ligo.caltech.edu/~gabriele.vajente/bruco_1159774937/
There is a lot of coherence a bit everywhere:
The "jitter noise" above 100 Hz shows a lot of coherence with many signals, of different origins. Most of the IMC WFS signals are coherent, for example: IMC-WFS_A/B_DC_PIT/YAW_OUT (fig. 5 and 6).
The most interesting coherence is however with the intensity stabilization: PSL-ISS_PDA_REL_OUT and PSL-ISS_PDB_REL_OUT shows quite large coherence, as well as the ISS control signal: PSL-ISS_AOM_DRIVER_MON_OUT. It seems that PDA and PDB (first loop ISS) are completely dominated by what the ISS second loop is doing (as shown by the control signal). The coherence with DARM in the 100-1000 Hz region is very close to one. See fig. 7 and 8.
Note that in the same 100-1000 Hz region, the coherence with PSL lab accelerometers is also significant, but mostly on the peaks (fig. 9)
En passant, a narrow feature at 56.75 Hz and 113.50 Hz are coherent with EX magnetometers (PEM-EX_MAG_EBAY_SEIRACK_X/Y PEM-EX_MAG_VEA_FLOOR_Y/Z)
I selected the channels with the largest coherence from the BruCo report, and run a multicoherence code.
chnames = {'H1:LSC-MICH_OUT_DQ', 'H1:LSC-SRCL_OUT_DQ', 'H1:LSC-PRCL_OUT_DQ', ...
'H1:ASC-AS_B_RF45_Q_YAW_OUT_DQ', 'H1:ASC-OMC_B_YAW_OUT_DQ', 'H1:ASC-OMC_B_PIT_OUT_DQ', ...
'H1:LSC-REFL_A_RF45_I_ERR_DQ', 'H1:LSC-REFL_A_RF9_Q_ERR_DQ', 'H1:IMC-WFS_A_DC_PIT_OUT_DQ', ...
'H1:IMC-WFS_B_DC_PIT_OUT_DQ', 'H1:IMC-WFS_A_I_YAW_OUT_DQ', 'H1:IMC-WFS_A_Q_YAW_OUT_DQ', ...
'H1:PSL-ISS_AOM_DRIVER_MON_OUT_DQ', 'H1:PSL-ISS_PDA_REL_OUT_DQ', 'H1:PSL-ISS_PDB_REL_OUT_DQ', ...
'H1:PSL-ISS_SECONDLOOP_RIN_INNER_OUT_DQ', 'H1:PSL-ISS_SECONDLOOP_RIN_OUTER_OUT_DQ', ...
'H1:PSL-PMC_HV_MON_OUT_DQ', 'H1:IMC-IM4_TRANS_SUM_OUT_DQ', ...
'H1:PEM-CS_ACC_PSL_TABLE1_X_DQ', 'H1:PEM-CS_ACC_PSL_TABLE1_Y_DQ', 'H1:PEM-CS_ACC_PSL_TABLE1_Z_DQ', ...
'H1:PEM-CS_ACC_PSL_PERISCOPE_X_DQ'};
The code take into account the cross-coherences between channels and produce the total coherence and an estimate of the noise projection, base on that coherence. The last figure (10) shows this coherence and the projection into the DCPD signal. A lot of noise can be explained by the coherences.
Just a quick note: Since I was running a2l many times during last night's lock, there isn't a lot of time that the lines aren't there. The 10 min that Gabriele chose include the lines. This doesn't change any conclusions except the peaks right around 20Hz.
Anyhow, Gabriele is going to take a quick look at the next lock, after I left for the night just in case.
Analysis results for the next lock are available here:
https://ldas-jobs.ligo.caltech.edu/~gabriele.vajente/bruco_1159781417/
No much difference, except that now DHARD_PIT is more relevant, see plot.
So, apparently Peter went into the PSL this morning and adjusted the HWP to give us more power incident on the rotation stage. However, this was not communicated to commissioners / people in the control room, so the ISC_LOCK guardian was still requesting 60W. With the hardware change, this was actually giving us ~60W into the vacuum. Something in the ASC didn't like this, and we lost 2 locks after ~1 hour each, with something drifting away.
EDIT: I guess some commissioners did know that we were getting 60W and decided to try running with it, we just didn't think it would have such a deleterious effect on the ASC.
The half waveplate before the IO EOM was adjusted to yield a maximum of 60W as displayed by the Ops Overview MEDM screen. Said activity was performed under the watchful gaze of the day operator, who was also my interlocutor whilst the waveplate was adjusted. So the power table looks like ...
Requested power | Indicated power |
---|---|
60 | 59.7 |
50 | 54.5 |
40 | 43.5 |
25 | 27.4 |
2 | 2.2 |
The only oplev which is furthest off (approaching -10urad) is the HAM2 oplev (pit & yaw). This closes out FAMIS#4696.
Nothing here looks out of the ordinary.
J. Kissel, S. Karki As we've done in O1, we're creating a high-frequency ( > 1 kHz ) excitation via PCALX whose frequency is changed over long-duration in order to map out the interferometer's sensing function out to as high as is needed for burst and binary neutron star coalescence searches. For quite some time now (since July! see LHO aLOG 28301), this line has been gathering data at 3501.3 [Hz]. We haven't moved it because the IFO's duty cycle has been low, the power level has been inconsistent, and our person power has been limited. Today is the day! I've resumed moving this line, following the schedule posted by Sudarshan in LLO aLOG 28070, which I repeat here for convenience: Frequency Planned Amplitude Planned Duration Actual Amplitude Start Time Stop Time Achieved Duration (Hz) (ct) (hh:mm) (ct) (UTC) (UTC) (hh:mm) --------------------------------------------------------------------------------------------------------------------------------------------------------- 1001.3 35k 02:00 1501.3 35k 02:00 2001.3 35k 02:00 2501.3 35k 05:00 3001.3 35k 05:00 39322.0 Oct 06 2016 18:39:26 UTC 3501.3 35k 05:00 39322.0 Jul 06 2016 18:56:13 UTC Oct 06 2016 18:39:26 UTC months 4001.3 40k 10:00 4301.3 40k 10:00 4501.3 40k 10:00 4801.3 40k 10:00 5001.3 40k 10:00 Several things to note: - The line frequency was changed in the middle of the lock stretch. - This lock stretch has been with the PSL power at 58.7W (we hope to run ER10 / O2 at 50 W). - Alignment of SRC optics is being slowly changed by commissioners - Robert has also been playing with Intensity Noise coupling, which is currently limiting the sensitivity at these high frequencies, so the SNR of the line may be varying quite wildly.
The past and current lock stretches at 60 W were unintentional consequences of a readjustment of the PSL HPO output waveplate without changing the power request back to 50 W (which had been changed to be 60 W yesterday when it was identified that the HPO wasn't putting out enough juice; see LHO aLOG 30239 and LHO aLOG 30260). We've now, mid-lock readjusted the power back down to 50W, so we expect to return to normal ER10/O2-like operation. So the CAL lines should be measured beyond this point.
Both HWSX and HWSY centroid refernces re-initialized after IFO unlocked for 2 hours. ITMs, BS, and SR3 are all aligned.
16:49 Re-initialized HWSX centroids ref
16:51 Re-initialized HWSY centroids ref
Summary: Repeating the Pcal timing signals measurements made at LHO (aLOG 28942) and LLO (aLOG 27207) with more test point channels in the 65k IOP model, we now have a more complete picture of the Pcal timing signals and where there are time delays. Bottom line: 61 usec delay from user model (16 kHz) to IOP model (65 kHz); no delay from IOP model to user model; 7.5 usec zero-order-hold delay in the DAC; and 61 usec delay in the DAC or the ADC or a combination of the two. Unfortunately, we cannot determine from these measurements on which of the ADC or DAC has the delay. Details: I turned off the nominal high frequency Pcal x-arm excitation and the CW injections for the duration of this measurement. I injected a 960 Hz sine wave, 5000 counts amplitude in H1:CAL-PCALX_SWEPT_SINE_EXC. Then I made transfer function measurements from H1:IOP-ISC_EX_ADC_DT_OUT to H1:CAL-PCALX_DAC_FILT_DTONE_IN1, H1:IOP-ISC_EX_MADC0_TP_CH30 to H1:CAL-PCALX_DAC_NONFILT_DTONE_IN1, and H1:CAL-PCALX_SWEPT_SINE_OUT to H1:CAL-PCALX_TX_PD_VOLTS_IN1, as well as points in between (see attached diagram, and plots) The measurements match the expectation, except there is one confusing point: the transfer function H1:IOP-ISC_EX_MADC0_TP_CH30 to H1:CAL-PCALX_DAC_NONFILT_DTONE_IN1 does not see the 7.5 usec zero-order-hold DAC delay. Why? There is a 61 usec delay from just after the digital AI and just before the digital AA (after accounting for the known phase loss by the DAC zero-order-hold, and the analog AI and AA filters). From these measurements, we cannot determine if the delay is in the ADC or DAC or a combination of both. For now, we have timing documentation such as LIGO-G-1501195 to suggest that there are 3 IOP clock cycles delay in the DAC and 1 IOP clock cycle delay at the ADC. It is important to note that there is no delay in the channels measured in the user model acquired by the ADC. In addition, the measurements show that there is a 61 usec delay when going from the user model to the IOP model. All this being said, I'm still a little confused from various other timing measurements. See, for example, LLO aLOG 22227 and LHO aLOG 22117. I'll need a little time to digest this and try to reconcile the different results.
By looking at the phase of the DuoTone signals we can constrain whether there is any delay in ADC side (like Keita's analysis here). The DuoTone signals are desgined such that the two sinusoidal signals 960 Hz and 961 Hz will be maximum at the start of a GPS second (and also in phase with each other). To be presice, the maximum will be 6.7 µs delayed from the integer GPS boundary (T1500513). The phase of 960 Hz signal at IOP (L1:IOP-ISC_EX_ADC_DT_OUT) is -92.52 degrees with respect to GPS integer boundary (LLO a-log 27207). Since the DuoTone signal is supposed to be maximum at GPS integer boundary i.e, it is a cosine function, this corresponds to -2.52 degrees (estimate of 92.52 assumes it is a sine function) phase change. Converting this phase change to time delay we get 7.3 µs. Since there is an inherent 6.7µs delay by the time the DuoTone signals reaches the ADC, we are left with only 0.6 µs delay possibly from ADC process (or some small systematic we haven't accounted for yet). This is what Keita's measurements were showing. Combing this measurment and above transfer function measurments we can say that we understand the ADC chain and there are no time delays more than 0.6 µ in that chain. This also suggest that the 61 µs delay we see in ADC-DAC combination exist completely in DAC side.
The DuoTone signals are sine waves, so a minor correction to Shivaraj's comment above, the zero-crossing corresponds to the supposed GPS integer second. I looked at a time series and observe that the zero-crossing occurs at ~7.2 usec. Since the analog DuoTone signal lags behind the GPS second by ~6.7 usec, I can confirm that the ADC side has essentially no delay. Thus, the 61 usec seen through the DAC-ADC loop is entirely on the DAC side. Attached is a time series zoom showing the zero crossing of the DuoTone signal.
When using dtt to make a transfer function measurement between an IOP model and a user model, one has to keep in mind that dtt does another decimation silently. This is due to dtt trying to match the number of data points between two models. Fortunately, this does not seem to affect the phase, see my note at https://dcc.ligo.org/T1600454.
Updated the timing diagram for consistency with other timing measurements (LHO aLOG 30965). See attached PDF to this comment.