The first unlock of this morning was manual (by error).
At 07h57 UTC unlock due to DIFFp high gain oscillation (plot 1). This was due to the servo of the DIFFp, which was working up to LN1 (since after that no coherence was visible due to the lowering of the line, which stops the servo). Unfortunately in the OMC lock phase the alignment loop is not optimal, we observe a transient in which the SR is aligned, then when the SR is aligned back in LN1 the sideband increase and the absence of DIFFp servo made the gain of the loop too high causing the unlock.
The solution implemented is to open the SR alignment loop after CARM 1f and close it back at LN1 with a slow ramp. see Figure 1 and 2.
ALS NARM: since the ramp was not scanning enough to find the TEM00, we changed the vco ramp set from 0.2 to -0.1 and vco ramp amp from 0.4 to 0.8
In LN1 we had to increase the DIFFp lines ampl for tx and ty from 1e-4 and 1e-3 to 2e-4 and 2e-3 because there was poor coherence with the line to let the servo to work during the change of modulation index for 56MHz (we have put back them to the standard config).
The purpose of the shift was to increase the modulation amplitude of the 56MHz and 6 MHz to 15 dBm and check if we could gain at low frequency. We removed the clipping on the SRCL set to be able to compare the different situations (now it is at 40). It was impossible to improve the sensing noise nor the sensitivity. We also tried to decrease the 56MHz to have the quadrature smaller, but still no change at all was visible (plot 3). The trend is visible in figure 4.
We also have tuned the Fmoderr with the calibration done yesterday but we were already at the zero. The calibration is visible in Figure 5.
We also tried the test of balancing the sidebands putting a MICH offset. See figure 6 After a while EPRB PC singal disappeared.
Moreover we tested the more perfomance filter for DIFFp ty which works correctly but I reverted the engagment since it is not yet manageble by the automation and we can not acquire DIFFpty with that loop. The effect on rms is visible in Figure 4.