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Adaptive Optics Facility
4 LGSF


Four Laser Guide Star Facility (4LGSF)

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

Laser Clean Room

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.

Laser Clean Room

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.

 

Lasers

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, UK, Toptica (D) and the Russian branch of the company Volius. ESO has so far reached 2.9W CW at 589nm in its lab, aiming to reach full power in the second half of 2006.

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.

 

Launch Telescopes

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.

Launch Telescopes on Centerpiece

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.

 

LGS Diagnostic System

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.

4LGSF laser diagnostic system

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.


The MACAO-VLTI system is a 60 element curvature AO system operating at the Coudé focus of one of the VLT UTs delivering a corrected wavefront to the VLTI delay lines after reflection off the dichroic M9. The corrective optics consists of a deformable mirror with 60 actuators mounted on a tip/tilt stage situated at M8 in the Coudé train. The Curvature Wavefront Sensor is based on a 60 element lenslet array feeding fibers connected to 60 APD modules; the CWFS is hosted in a WFS box mounted on an X-Y table standing on the Coudé floor below M9. MACAO-VLTI is designed to operate only with natural guide stars.For bright sources (mv 8th mag). MACAO delivers 55% Strehl ratio on the sky for a 0.8" seeing (64% was reached in the laboratory on 0.65" seeing and the system was specified to provide at least 50% Strehl ratio @2.2um on axis under median seeing conditions of 0.65"). For faint sources 10% Strehl has been attained on the sky on mV=16.5 mag star with 0.55" seeing. (specification was at least 25% Strehl ratio @2.2um on a mV 15.5th mag star in 0.65" seeing). An IR output beam stability of 4 mas (ignoring residual refraction) of star position errors has been observed in the laboratory. An interface is provided to allow feedback from an IR tip/tilt camera located in the interferometric lab under the control the VLTI to compensate for these errors.

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 Team

 

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
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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