\documentclass{ligodoc}
\usepackage{hyperref}
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\author{J. Romie and N. Robertson} 
\ligodccnumber{T}{09}{00156}{v3}{I}
\title{Reply to ``OMC Suspension FDR comments from reviewers''}


\begin{document}

\section{Introduction}

\textcolor{red}{\emph{The reviewees' replies to the reviewers comments are
    included below, italicised and highlighted beneath the
    corresponding comment.}}

The Output Mode Cleaner (OMC) Suspension (SUS) Final Design Review
(FDR) committee met March 13, 2009 to prepare preliminary questions
for the OMC-SUS design team.  The committee reviewed documents on the
Final Design Review page at
\url{http://ilog.ligo-wa.caltech.edu:7285/advligo/OMC\_Suspension/Final\_Design\_Review},
specifically T0900060-v1.pdf and T0900049-v1.pdf.  We were very
impressed with the quality of the documentation and the performance of
the OMC-SUS.  We believe some additional measurements will complete
the FDR package and allow us to quickly approve the OMC SUS for
advLIGO.

Since the OMC-SUS was designed and installed for Enhanced LIGO, there
was no formal Preliminary Design Review.  Consequently, this FDR may
exceed the bounds of a traditional FDR as laid out in M050220-09.  The
installed OMC suspensions provide an excellent opportunity to test
against actual interferometer performance and mitigate risks to
advLIGO.  Before the review committee approves the OMC-SUS design for
advLIGO, we'd like to see the test suite expanded and the noise
contributions from OMC motion shown to be negligible as calculated.

The advLIGO Output Mode Cleaner will differ from the Enhanced LIGO
OMC, perhaps significantly.  The new OMC may not be the same mass, nor
have the same electronics and cabling requirements.  While the major
structural components will remain unchanged, a new payload mass would
require new blade springs.  Consequently, development of an improved
blade spring procurement process (per E0900023?)  is required for the
OMC-SUS.

The remainder of this note presents the review committee's detailed
requests for the Final Design Review.

\section{Relevant documents}

\noindent
\href{https://dcc.ligo.org/DocDB/0000/M050220/001/M050220-09.pdf}{\textbf{M050220-09}}
``Guidelines for Advanced LIGO Detector Construction Activities''

\noindent
\href{https://dcc.ligo.org/cgi-bin/private/DocDB/ShowDocument?docid=660}{\textbf{T0900060-v1}}
``OMC Suspension Final Design Document''

\noindent
\href{https://dcc.ligo.org/cgi-bin/private/DocDB/ShowDocument?docid=870}{\textbf{T0900049-v1}}
``Output Mode Cleaner Suspension Lessons Learned,  Changes Needed \& Problems \& Concerns''

\noindent
\href{https://dcc.ligo.org/cgi-bin/private/DocDB/ShowDocument?docid=922}{\textbf{T0900080-v1}}
  ``OMC Suspension Advanced LIGO Test Plan''

\noindent
\href{https://dcc.ligo.org/cgi-bin/private/DocDB/ShowDocument?docid=847}
{\textbf{T0900071-v1}} ``Results of Damping Tests for the LLO OMC''

\noindent
\href{https://dcc.ligo.org/cgi-bin/private/DocDB/ShowDocument?docid=1303}{\textbf{T0900114-v2}}
``OMC Suspension FDR comments from reviewers''



\section{Detailed comments}

\subsection{OMC Interface Cables}

The OMC electrical cables are the least understood aspect of the
OMC-SUS and therefore present the highest possible remaining risk.
The Final Design Document offers two somewhat exclusive views: on the
one hand modeling predicts a minimal impact from the cabling, on the
other hand a 30-fold increase in mode coupling and significant damping
is attributed to the cabling.  The committee would like to see this
issue resolved before advLIGO.  Specifically, the committee has the
following questions and suggestions:

\begin{enumerate}
\item In the worst case model, do the electronics cables compromise the
  suspension performance to the point of violating the noise
  requirements?

\textcolor{red}{\emph{We have been doing further modeling which suggests that the
  natural damping seen is close to the level we might expect from the
  effect of the cabling. We will be able to comment further on whether
  the performance obtained violates the noise requirements when such
  requirements have been supplied to us.}}


\item The original OMC-SUS designed called for cable routing tied to
  the intermediate mass before connecting to the structure.  Could
  this feature be re-incorporated into the intermediate mass?  If so,
  how would we prevent the problems we had the first time around?
  Assuming similar cable stiffness, what does modeling tell us about
  the impact of such a change?

\textcolor{red}{\emph{We strongly advise against returning to routing the cable via
  the intermediate mass. When this was done before we found that not
  only was there coupling of modes, but also the cable significantly
  affected the DC alignment of the intermediate mass and hence also
  the OMC bench. Such misalignments were approximately as large as the
  maximum range of the OSEMs. The cables thus have a significant
  influence. This is not surprising given that they are relatively
  bulky and the intermediate mass is only 3 kg. We note that this
  experiment was done when there was a peek covering on the
  cabling. However even without this covering we would expect to see
  an effect. One way to mitigate this might be to increase the mass of
  the intermediate mass, but that would be a very significant design
  change.
}}

\item The electronics cables are shielded bundles of wire with
  non-zero twist that may relax with time.  Is this an issue?  If so,
  perhaps an ``egg dipper'' similar to that found on the quad
  suspension could be incorporated to explicitly guide the cable
  routing and ensure excess rubbing doesn't appear after installation.

\textcolor{red}{\emph{We have no evidence for or against relaxation with time being an
  issue. We are unclear which particular area of rubbing the committee
  is referring to. We could incorporate an "egg dipper" arrangement if
  this helps to reduce such rubbing.}}

\item For eLIGO, the OMC design made ``reasonable'' design choices to
  minimize stiffness but did not aim to surpass a specific performance
  - perhaps there is room for improvement if SUS/ISC can get together.
\item Cable/no-cable tests with the installed hardware can be done in
  vacuum after Enhanced LIGO.  Such a test (or similar) should be used
  to quantify the impact of the electronics cables before advLIGO.  We
  should all get together on this.

\textcolor{red}{\emph{We are happy to help with this.}}

\end{enumerate}

\subsection{Modes and transfer functions}

The qualitative agreement between the simulation and measurement as
shown in Figure~6 is very impressive.  There is less detailed
quantitative comparison in T0900060 making it difficult to evaluate
whether the suspension meets the requirements.  The committee has the
following questions and suggestions:

\begin{enumerate}
\item Explicitly measure the transfer functions from the ISI to the
  OMC in units of meter / meter and radians / radian so that seismic
  noise estimates can be made directly from measured data instead of
  relying on the models shown in Figures 4 and 5. The upcoming
  downtime at LLO would be an appropriate time there and SJW will look
  at this March 22-26 at LHO.
\item The original ISC requirements may not include all the relevant
  physics.  An explicit measurement of the coupling of OMC motion to
  DARM, followed by an extrapolation to advLIGO will eliminate the
  risk associated with the OMC suspension.  SJW will look
  at this March 22-26 at LHO.
\item The OMC-SUS to ISI clamping should be improved during the next
  HAM6 vent and the predicted 140 Hz lowest mode observed.  This is
  already planned by the commissioning teams for the next LLO and LHO
  vents. Does the 103 Hz modes observed currently impact ISI servo
  design?

\textcolor{red}{\emph{This is a question for our SEI colleagues. I have asked Brian
  L.}}

\item Extend the transfer function measurements to high frequencies.
  This has at least two advantages: possibly revealing the excess
  damping in from the electronics cables which are invisible in the 20
  Hz transfer functions shown, and checking for electronics cross
  coupling and failures at higher frequencies. SJW will look
  at this March 22-26 at LHO.
\item The mode frequency degeneracy makes a complete modal basis
  control of the OMC difficult and unintuitive.  Can anything be done
  in the advLIGO OMC-SUS to break these degeneracies?

\textcolor{red}{\emph{We assume the degeneracies referred to are in the two horizontal
  directions (longitudinal and transverse). These are very similar
  since the wires are vertical. Angling the wires at either or both
  stages would change the frequencies slightly. However to do this
  would require significant design changes to clamps, wire jigs and
  attachment points and (for the lower stage) method of attachment to
  the bench. It is not clear that a modal basis control is needed.}}

\end{enumerate}


\subsection{Electronics}

The OMC-SUS electronics package is in very good shape.  The committee
has the following questions and suggestions:

\begin{enumerate}

\item
The current OMC-SUS relies on the CDS borkspace watchdog model.  This
is inadequate: only 5 DOFs are monitored, the code is un-reviewed, and
the watchdog does not conform to T080127 as implied.  The ISI watchdog
has recently been reviewed and should be modified for use in the
OMC-SUS as a part of this FDR.

\textcolor{red}{\emph{Watchdog-- The ISI watchdog can be modified and used in the
  design as the reviewers suggest.  }}

\item
Recent ISC work has re-discovered many issues in dealing with ADC and
DAC systems.  The committee would like to see the in situ spectra for
the ADC and DAC along with the advLIGO whitening and de-whitening
filter designs to ensure that an appropriate digital dynamic range is
used and digitization errors are minimized. These spectra may be taken
at the filter module input immediately after the ADC and at the filter
module outputs preceding the DACs, eg. L1:SUS-OMC\_TOP1\_IN1 and
L1:SUS-OMC\_T1\_ACT\_LIMIT.

\textcolor{red}{\emph{Agreed. This measurement can and should be made.}}

\item The BUF634 op amp in the coil driver output will be discontinued
  in the future.  Look for changes to the coil drivers in the future.

\textcolor{red}{\emph{This is a known problem. The coil driver board will need to be
  redesigned to use a different buffer. We are presently using the
  OPA544 on the triple coil drivers. Once we verify the performance of
  this part we can change the coil driver design accordingly. }}

\end{enumerate}

\subsection{Re-use of existing suspension parts}

The design team has carefully identified potential issues with the
re-use of existing parts.  The committee has the following questions
and suggestions.

\begin{enumerate}
\item SJW has conferred with the VRB representative Mike Zucker
  regarding the existing 303 stainless parts.  Future parts for the H2
  suspension and potential redesigns should be made from vacuum
  approved materials.  The existing parts may be grandfathered into
  advLIGO. 

\item Unless the design team demonstrates that the non-linear
  couplings induced by bent springs compromises the performance, the
  review committee is satisfied with the current blades.  However, the
  procurement difficulties experienced by eLIGO seemed to limit the
  installation options at that time.  In keeping with the new blade
  spring development, replacement blades should be fabricated for both
  OMC suspensions assuming the current mass (or slightly higher).  The decision
  to replace the blades may be deferred.

\item Nickel plating and corrosion resistance may be a significant
  problem.  As mentioned above, replacement blades should be
  fabricated, including nickel plating so the blades may be replaced
  if corrosion is observed or if the OMC suspension is  left
  outside of vacuum for extended periods.

\item The SUS transfer functions should be repeated at intervals to
  evaluate long term consequences of shot-peening.  No further action
  is required at this time.

\item Please detail the changes between LLO and LHO.  Unless the
  changes provide significant operational enhancement, the committee
  does not \emph{a priori} see any requirement to rework the LLO
  suspension.

\item Please detail the IO chassis and cabling changes envisioned.

\textcolor{red}{\emph{The new IO chassis is in the prototype stage of design. Once the
  design has be completed and tested the details can be made
  available. The design should be more mature by late summer 2009. }}

\end{enumerate}



In addition to the issues raised by the design team, the committee
strongly recommends that the OSEM shadow sensor electronics be
modified to conform to the initial LIGO usage.  Specifically, the
shadow sensor signals should have a gain and offset such that the
digitized signal extends from -10 to 10 volts (or similar) and the
nominal, centered OSEM position returns 0 volts.

\subsection{Documentation}

A few pieces of documentation weren't linked to the FDR WIKI page.
The review committee would like to see a subsystem functional block
diagram, links to software design, and final specifications.  The
production plans are unclear or inaccessible by the review team: how
many suspensions are required?  Similarly, we have found no cost
estimates.  Once production has started, what is the marginal cost for
additional spring sets?  For replacement intermediate masses?

\textcolor{red}{\emph{Software design: This can be obtained from LLO. (TBD)
Block diagram: 
i)  a signal flow diagram for the electronics is on the wiki, see
\url{https://dcc.ligo.org/DocDB/0000/D0900339/001/D0900339-v1.pdf}
There is also a block diagram on the wiki that shows the ISI and SUS controls for the OMC, see
\url{https://dcc.ligo.org/DocDB/0000/D0900316/001/D0900316-v1.pdf}
Cost information and procurement plan have been provided separately
}}

\section{Conclusions}

The OMC Suspension design team has put together an excellent design
and extensive documentation.  The majority of comments above should be
considered non-critical suggestions.  The few issues that are
critical: test the cable damping or calculate that it does not compromise
the noise performance, measure the ISI to OMC-SUS transfer function in
meter per meter, excite the OMC motion and observe DARM response, and
demonstrate a cantilever spring fabrication technique.  The upcoming
shutdown at LLO provides a great opportunity to monopolize ISI and
HAM6, completing the testing.

\end{document}


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