This morning after the meeting Thomas and I actuated the motorized rotation stage in order to attenuate the laser power in the H1 PSL path. The shutter for both the main PSL beam and the ALS pickoff has been closed, locked and tagged. However, we also decided to decrease the power leaving the PSL table so that 8 W of light is not hitting the shutter for the duration of the vent.
The MEDM interface for the rotation stage has multiple functions, but the two main calls are to REQUEST ANGLE for the motorized stage or to REQUEST POWER being output after the light passes through the waveplate. Currently only the REQUEST ANGLE function is useful because of some missing calibration data. I will work to get this fixed so we can request a specific power or use the GO TO MINIMUM POWER function.
For now we plotted the power output as we rotated the stage and then manually requested an angle corresponding to the minimum. 63 degrees in this case, which corresponds to approximately 50mW of light entering the PSL light pipe. note that the ALS pickoff is before the motorized stage, so that path still has somewhere around 250mW of 1064nm light.
see attached for the plot of power and rotation angle
A certificate has expired on the local CDS LDAP replica which is preventing LIGO.ORG logins on some of the control room workstations (depending on when they were last rebooted, or last connected to the LDAP server). For now, if you cannot log in to a workstation with your personal login, use the controls account instead. I am looking at a workaround until the new certificate is issued, but that will take a while longer to roll out.
I have implemented a temporary workaround for opsws0-10 in the control room to allow LIGO.ORG logins, so they should work again. On any other systems, use the controls account if your login does not work until further notice. Access from offsite via lhocds.ligo-wa.caltech.edu is unaffected (but you will still need to keep in mind the above if using lhocds to access any internal CDS hosts).
In light of the upcoming vent, it seemed like a good time test the ability of the test mass optical levers to recover from the venting, swapping and re-pumpdown. I've recentered the optical levers on 2014-06-02 17:05 UTC with the following status:
SUS values:
ITMX_Pit = 38.7
ITMX_Yaw = -48.9
ITMY_Pit = 193.4
ITMY_Yaw = -181.1
HEPI Isolated and biases are:
ITMX_RX = -6020
ITMX_RY = -45350
ITMX_RZ = 71250
ITMY_RX = 44920
ITMY_RY = 48020
ITMY_RZ = -23500
ISI Stg1 Isolated and biases are:
ITMX_RX = -17600
ITMX_RY = 27450
ITMX_RZ = 30450
ITMY_RX = 9760
ITMY_RY = -28600
ITMY_RZ = 6760
ISI Stg2 Isolated and biases are:
ITMX_RX = -4565
ITMX_RY = -680
ITMX_RZ = 7744
ITMY_RX = 19623
ITMY_RY = -12484
ITMY_RZ = 7496
LVEA transitioned to laser SAFE
Teams taking fiducial measurements (ITMs/ETMs/OpLevs)
Ready to vent all three corner station volumes after lunch
Good results from Thomas measurements on the stability of RH over the weekend
HAM4/5 doors and HAM6 septum in place
HAM6 SLED ready to install, on hold for now
need visual inspect on HAM6 cabling lengths
Apollo restoring beer garden cleanroom---coupling with BSC1/3
installation of TCS table stops on hold
need to lock HEPI for BSC1/3 due to potential contact with HEPI crossbeams
need to protect TCS mirrors during in chamber work
The particulate mobility experiment that is mounted to HAM 3 is back up and running. It will be running for the next 3 days to make sure the entire vent cycle is captured.
Betsy, Sheila, Keita, Arnaud, Thomas
Here is a snap shots of the current alingment offsets. This alingment was checked quickly this morning, both of the arms are flashing green so the ITMs are within a urad or so of alinged.
We noticed that the ailngment of ITMY was off by about 8 urad in pitch from the saved offset, this seems to be because turning on and off the ring heater changes the ailngments. Attached are trends of the OpLevs durring the ring heater stress test this weekend, the itms moved by 2-5 urad in yaw, and both moved by about 30 urad in pitch. The third screenshot shows how the pitch changed as the ring heater power cycled.
@DetChar -- can you grab calibrated ASDs of the optical levers before and after the ring heaters are on full blast? It looks like they not only displace the optic in angle, but also add noise. It would be good to quantify this early, so we can fix it!
I forgot to check this. https://dcc.ligo.org/LIGO-T1100184 Phil Willems wrote a document (T1100184) that predicted around 0.9urad of pitch per Watt of RH power. We applied 27W of power, so the Spurious Willems Pitch is around 24urad. This seems consistent with what was seen. It's worth a more detailed look though. I can't explain the 8urad offset between the start and finish.
From Jeff's request I've taken a look at the Oplevs before, during and after the heaters were on and found their ASDs (1st plot). These ADSs are taken over 10 minutes and the times are noted in the legend. I specifically chose times where the ITMY ISI ODC is reporting a good state. In addition the BLRMs look normal and similar for all three times. I also found the ground motion ASDs for these times (2nd plot) to reconfirm the ground motion is similar for all three times. Conclusion - the ASDs for the Oplevs look very similar before, during and after the heaters are on; they don't appear to add extra noise. There is perhaps an extra peak between 7-8Hz in the YAW when the heaters are on but other than that nothing stands out.
There is also a DC power level difference between states before after the weekend stress test. Based on the channel H1:TCS-C_RH_Y_LOWERCURRENT and Aidan's note of 27 W in the ramp up state, the forementioned DC offset correspond to a power level difference of ~8 W (assuming 0.55 for the current level during stress test and 0.3 before the stress test and 0 after the stress test, obtained from the plot of H1:TCS-C_RH_Y_LOWERCURRENT; 27 * 0.3^2/0.55^2). From the dcc documnet noted in the Aidan's comment this correspond to ~8 urd difference we between the initial and end states. This also means that we probably have to make new reference with the current setting (of zero current), if desired.
The ITMY ring heater was set to 8W during the past commissioning period to correct for the fact that we had an ETM with ITM coating installed. This will be changed in the current installation phase. New references will be rquired when we have the new optics installed and aligned.
Also note, the ITMs that this ring heater test was performed on are hung from metal wires in stead of glass fibers. I wonder if this is what is making them more susceptible to steering errors when the ring heater is engaged... The current install is to swap these ITMs out for new units complete with glass fibers. Hopefully the ITMs won't be as susceptible to mispointing when on fibers if this is the case.
J. Kissel As Betsy indicates these ITMs are suspended via steel wire instead of fused silica fiber. This plays a difference in the compliance used in the Phil's calculation of the expected displacement in T1100184. Also, the Willems calculation uses a QUAD suspension model from T1000263 which is an out-dated model parameter set that was never confirmed against real measurements (which we now have). Also it's unclear which Stage / DOF to Stage / DOF was used to produce the "pitch coupling" of 0.154 [rad/Nm]. The mathematica notebook that is "available from the author" is regrettably *not* zipped up in the "Other Files" on the DCC card, so I can't confirm. The attached .pdf doesn't have the 0.154 anywhere in the document. However, assuming the compliance he used was pitch displacement of the test mass from pitch torque on the test mass, the values from the production quad model model (now confirmed against measurement) are Fiber: 0.141 [rad/N.m] (using the quadopt_fiber.m parameter set) Wire: 0.105 [rad/N.m] (using the quadopt_wirerehang.m parameter set) Willems quotes the displacement of the Center of Mass (CoM) as 1.47e-7 [m] for 11 [W] of ring heater power. Assuming the displacement is linear with ring-heater power (safe assumption??), that's 1.34e-8 [rad/W] The displacement one expects per Watt of Ring heater power from the Willems model of a displaced CoM is then Fiber: 1.34e-8 [m/W] * 40 [kg] * 9.8 [m/s^2] * 0.141 [rad/N.m] = 7.4064e-07 [rad/W] = 0.74 [urad/W] Wire: 1.34e-8 [m/W] * 40 [kg] * 9.8 [m/s^2] * 0.105 [rad/N.m] = 5.5154e-07 [rad/W] = 0.55 [urad/W] And therefore at max power of 27 [W], the ITMs should be displaced by Wire: 5.5154e-07 [rad/W] * 27 [W] = 1.4892e-05 [rad] = 15 [urad]. This is a factor of two less than what is seen in ITMX Pitch (the cleanest example). For ITMY, I don't think the test mass was allowed to reach equilibrium before the ring heater's power was changed during the power cycling, so it's more difficult to assess the displacement -- but I think it's much closer to 15 [urad] judging by when the test was turned off (presumably it was turned off to zero current, and not the equivalent of 8 [W] that it had been set to as Daniel indicates).
Jeff pointed out that the factor of two in the ring heater deviation could arise from the optical lever gain in ITMY being a factor of two smaller than ITMX. We trust the ITMX's optical lever calibration because its gain was measured using the baffle PDs and the entire 4km arm (noted in ALOG 10331) but it doesn't look like a similar procedure was done for ITMY, or at least we couldn't find an ALOG that indicated as such.
no restarts reported.
D. Hosken, G. Grabeel, T. Vo We were able to fix the ring heater chassis EtherCAT wiring by referencing the drawings. We initially turned both ITM ring heaters to 30 Watts at 6:46 PM PT but it seems as though the maximum power that the drivers can put out is ~15-16 Watts so we changed the script that Greg wrote to run the power at 13.5 Watts during the high power portion and .5 Watts in the low power portion. I'll come in tomorrow morning to run some trends and take some measurements. John verified in the first hour that there were no spikes in pressure.
Here's the past 17 hour trends, there doesn't seem to be much correlation between pressure and ring heater cycling. The test is going to run for about another 5.5 hours or so. Also, I've plotted one cycle at 17:17 UTC and you can see the voltage rise to a steady state in about 30 minutes or so as we would expect, which means that the temperature of ring heater in question is in fact getting hotter which changes the resistivity and the ring heater driver is reacting to that change. The current output is noisier and the X_UpperCurrent doesn't seem to follow this trend and I'm not sure why.
The RH driver is a current source. There's an internal servo that holds the drive current steady - hence it doesn't change as the RH resistivity changes.
Thanks Aidan. We've finished with the test, both ITM RHs are now off.
It looks like we will need to go in chamber at end X to fins IR on the QPDs. I searched for the beam today by locking ALS, and moving the picomotor for M4 to toward the position that Kiwamu et al found in February (alog 10091). This was fine for the Y direction, but in the X direction I only got about a quarter of the way toward the old position before the green transmitted power started to drop. One theory is that this could be the green clipping on the mount for M4 (TMS table drawing). After a little bit of searching around, I decided move the picomotors back to the position that we had set them to to restore the beam on the table.
The positions used to get IR onto the LSC PD from February until yesterday were 9267 X 1665 Y for M4. Today after moving the picomotor around quite a bit, I needed to use 27357 for X and -12616 for Y to restore the beam to the same position. So these numbers are meaningless as references.
If you remove the snout from the LSC TRX PD in air, there are two brighter green spots (with two very faint spots below them to form a square, right now the lower ones are clipped upstream). The one that is slightly brighter and on the side of the PD face that is closer to the chamber is the one that is co-linear with the IR, and could be used as a reference if we decide to send IR into the chamber from this path to align the QPDs.
Yesterday Daniel noticed that the beam was clipped on EX WFSA, but the beam was not centered either and we were in the middle of IR beam finding. Today I centered the beam and it was still clipped because the beam was coming to the WFS head at much shallower angle than it should be. I fixed it by tilting the WFS head.
I and Daniel went to EY and tested WFSB using AM laser, and we saw that some of the channels were a factor of 5 or so smaller than the others.
Eventually we tracked it down to the WFSB whitening chassis (S1101602) though I thought it was working OK on Thursday (https://alog.ligo-wa.caltech.edu/aLOG/index.php?callRep=12138),
We tested S1101601 that was pulled out earlier this week that was suspicious unit but was never conclusively diagnosed bad, and it didn't work. So we got another spare unit (S1101638) from the corner station and put it in.
What are in use now: S1101600 for WFSA, S1101638 for WFSB.
Bad units: S1101601, S1101602, S110163.
Bad ones are put on a table in EY.
model restarts logged for Fri 30/May/2014
2014_05_30 14:42 h1fw0
unexpected restart of h1fw0
John Worden, R. Weiss Vibration measurements of the beamtube with the new R10 insulation and aluminum jacket were made and described in the appended document. The new insulation reduces the acoustic coupling to the beamtube but not as well as the initial insulation. The data enables a more detailed estimate of the phase noise from the beamtube motion due to the faulty HR coatings of the new test mass mirrors. The DCC number of the document is T1400384.
Error in the document. Please see T1400384-v2 or LHO log entry 12232
(Keita, Daniel)
Today we measured and adjusted the gain/phase of the WFS RF signals. WFS_A looks fine, but WFS_B has segments 3 and 4 which are ~10x smaller than 1 and 2. Engaging DOF4 did result in a stable feedbakc but with a rather large offset. We added an offset to segment 4 of WFS_B to recover. Adding DOF3 did not result in a stable feedback.
Playing around with the individual pit/yaw offsets and the WFS DC centering one can find feedback topologies with all 4 DOFs engaged. However, they are susceptible to disturbances.
For this measurement the WFS offsets are:
Bias | WFS A | WFS B |
---|---|---|
Pitch | -2500 | -1600 |
Yaw | -5000 | 4700 |
First measurement shows an ETMY yaw misalignment by 1 µrad. The power drops by about 15%. The yaw offsets are of order 10,000 counts. We also see a significant pitch ofset. But, more importantly the DC offsets on the WFS heads are also very large. The WFS servo was off during the measurement.
The second plot shows the effect of moving the picomotor for WFS_B by about 0.2 in yaw and 0.3 in pitch. The resulting offsets are of order 7000. Since the WFS servo was off, there was no degradation of the cavity power.
When the septum was removed, the cabling between HAMs 5 & 6 were disconnected so the crew could deal with all the bolts. I asked FClara to reconnect the cables to the WHAM6 NW feedthru, SUS & ISC I think. I'm not familiar enough to distinguish these so I left those to him. When they are sorted out I will complete the cable/feedthru protecting. Meanwhile, HAM5 ISI sensors are live, don't disconnect any cabling, you'll have to cut zip ties to do so.
Installed SUS and ISC cabling to D3 flange of HAM6 (NW corner). Flange Cable Description D3-1C1 H1:SUS_HAM6-10 OMC TOP D3-1C2 H1:SUS_HAM6-11 OMC Right/Side D3-2C1 H1:ISC_HAM6-265 ASC_AS_A (WFS) D3-2C2 H1:ISC_HAM6-266 ASC_AS_B (WFS) Document D1300122, internal in-vacuum cabling calls out for cable ISC-265 and ISC-266 to be connected to flange D5-3C1 and D5-3C2. Document should be updated. Filiberto Clara
HAM6 NW Cables stress relieved and E-FeedThrus protected.