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Adaptive Optics Facility
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The 4LGSF is a required facility for the operation of the AO modules
being part of the AO Facility. It shall provides the laser guide stars
to allow wavefront sensing for the AO modules. It is based on sodium
(Na) laser triggering the resonance lines of Na at 588.9 and 589.6 nm
of the 10 km high atmospheric Na layer. It therefore implies that all
high order wavefront sensing of the AO facility is based on LGS and is
therefore subject to a number of typical laser guide star
problems/fetaures: cone effect, no tilt information, jitter correction
& beam return time, laser spot elongation etc. These are relevant
points being addressed in the design of the AO modules and 4LGSF.
The following sections describe the 4LGSF conceptual design.
| Built by: | ESO LGS Group |
| Project Manager: | Wolfgang Hackenberg (whackenb@eso.org) |
| Location: | Laser clean Room & Center
piece of UT4 (TBC) |
| Status: | Conceptual Design Review passed; now in preliminary design phase |
Contents |
The upgrade of the LGSF to 4 LGSF takes full advantage of the existing Laser Clean Room. As much as possible, the electronics cabinets are in the LCR, the interlock panel and the fibre laser sources are in the LCR, and most of the heating/cooling is confined to this space. The easy access to LCR helps in servicing and maintenance, and the numerous safety issues becomes more manageable.
The existing LCR was already dimensioned to host multiple lasers, in the LGSF project. Moreover, with fibre lasers the power consumption is much reduced. Hence very little modifications are required to the Laser Clean Room for the upgrade to 4LGSF.

Figure 1: The Laser
Clean Room is a
class 10000 volume, built under the UT4 Nasmyth A platform (opposite
side of
NACO). It hosts three electronics cabinets, one optical table to be
used for 4LGSF
maintenance, electric power, cooling liquid distribution and general
services.
There are connection points for cooling, LAN, compressed air, and
safety
measures such as a fire extinguishing system based on Inergen gas,
limited
access system for Class IV laser environments and anti-Earthquake
passive
measures. Small changes only are requested for the 4LGSF upgrade.
The baseline lasers are 1178nm
fibre Raman
lasers, which are frequency doubled to 589nm. The fibre delivers 20+W
CW at
1178nm, 1GHz linewidth. The frequency doubling is done via a single
pass on
PPSLT, a non linear crystal. The fibre laser is an on-going development
at ESO,
together with the companies IPF Technology Ltd,
The fibre laser system is contained in one 19 inch module; five of these units will be placed in the electronic cabinet next to the LCR entrance door. The polarization maintaining single mode fibre will reach directly the Launch telescopes, using a fireproof fibre cable and going through the altitude cable wrap up to the UT4 centerpiece. At each launch telescope, a small box contains the frequency doubling PPSLT crystal, its temperature controller and the frequency feedback control sensor. The frequency doubling unit is located at the Launch Telescope.
The 1178nm fibre laser and the frequency doubling units are part of the industrial laser delivery.
The four Launch Telescopes located on the centrepiece have demanding requirements. The projected laser beam quality has to be diffraction limited to guarantee the minimum LGS angular size, which imposes constraints on the optical train and calls for the maximum simplification possible. Care has to be applied for optics working at high power densities. This requirement coupled with the flexibility to point the LGS at 0, 60 or 330 arcsec off-axis, as required by MUSE and Hawk-I, has driven the choice of the Launch Telescope optics toward a refractive, single lens f/5 design, with the fibre laser output at its focal plane. We have explored also reflective designs, and came to the conclusion that a refractive solution is preferable. The first Eigenfrequency of the LTS has to be >60 Hz, in order to avoid LGS wandering and unwanted jitters. This imposes strict choices on the mechanical support structure of the LTS, which is in CFRP to ensure stiffness and reduce weight.

Figure 2: The four
Launch telescopes
of the 4LGSF baseline design are mounted on the UT4 centerpiece.The
singlet
large BK7 lenses are supported by a carbon fibre cone-shaped shell,
which
grants high rigidity and stability. The fibre laser output goes
directly at the
focal plane of the f/5, 500mm diameter lens.
Above the Launch telescope, there is a movable shutter curtain to protect the lens when it is not in use, and a long baffle (see Fig 3.4 below) to avoid as much as possible scattering light in the telescope environment. This is also to avoid that the telescope volume becomes at Class IV laser volume.
In operation, there can be the diagnostic system in or not. A motorized flipper mirror can optionally send the output beam to a Coherent LM-45 calibrated power-meter, to measure the output beam power.

Figure 3: Operation
mode with the Beam Diagnostic System
on. 1% of the intensity feeds the diagnostic path. If the beam is
deflected to
the Bolometer by the flipper mirror, the system can be diagnosed in
daytime as
well.
MACAO can close the AO loop on point sources and extended objects with a size < 2.5", up to a maximum of seeing 1.0" @0.5um. The MACAO system can operate with the NGS on-axis or, by tracking the X-Y table on which the CWFS box sits, up to 1' off-axis. During sky tests in late April '03 the object Frosty Leo has been succesfully observed (extend ~3") and bright stars have been observed in extremely bad seeing conditions (~2-3") proving the flexibility and stability of MACAO-VLTI.
MACAO includes a viewing camera within the WFS box, which allows the performance of the system to be monitored during daytime operations using an artificial source and may also be used as a 10" diameter FOV acquisition camera for the VLTI.
The MACAO software provides automatic guide star acquisition and AO loop optimisation procedures. During closed loop operation it provides low frequency diagnostics via the OLDB and high frequency diagnostics via the VLTI reflective memory network. At the end of an observation a FITS file containing time tagged data characterising the AO correction during the observation is made available to the VLTI.
For the VLTI, up to four Coudé foci will be equipped with MACAO systems which are coordinated with the other subsystems of the VLTI and the TCS by the VLT interferometer supervisor software (VLT ISS) to perform interferometric observations.
| Project Manager & System
Engineer |
Wolfgang Hackenberg |
whackenb@eso.org |
| Project controller & design |
Domenico Bonaccini-Calia |
dbonacci@eso.org
|
| Mechanics | Ronald Guzman Heinz Kotzlowski Jutta Quentin |
rguzman@eso.org hkotzlow@eso.org jquentin@eso.org |
| Mechanical Analysis |
Marco Quattri | mquattri@eso.org |
| Optics | Domenico Bonaccini-Calia |
dbonacci@eso.org |
| Electronics | Ivan M. Guidolin C Dichirico Gert Fischer |
iguidoli@eso.org cdichiri@eso.org gfischer@eso.org |
| Software |
Antonio Longinotti |
alongino@eso.org
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| Lasers | Yan Feng Luc Taylor |
yfeng@eso.org ltaylor@eso.org |
| Opto-Mechanical Integration/Mechanics | Armin Silber |
asilber@eso.org |
| Paranal Interfaces |
Mario Tapia |
mtapia@eso.org |
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