GRAVITY acquisition camera

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GRAVITY acquisition camera Narsireddy Anugu 1, António Amorim, Paulo Garcia, Frank Eisenhauer, Paulo Gordo, Oliver Pfuhl, Ekkehard Wieprecht, Erich Wiezorrek, Marcus Haug, Guy S. Perrin, Karine Perraut, Christian Straubmeier, Wolfgang Brandner 1 CENTRA/SIM, University of Porto 14 th January, NICE

GRAVITY: phase-reference interferometer Target Reference 5 nm 500 µm 10 µ arcsec

GRAVITY subsystems Adaptive optics Metrology system Integrated optics Fringe tracker Fiber coupler and laser guiding system Acquisition camera

Why acquisition camera: To stabilize pupil motions

Why acquisition camera (2): atmospheric tip-tilts In GRAVITY the coherent beam combination implemented with fiber fed integrated optics Problems: 1. Flux injection 2. Astrometric error

Technical requirements to achieve GRAVITY aims To achieve 10 micro arcsec astrometry, GRAVITY requires 1. Field stability (error 2 mas) 2. Pupil stability: lateral position error 4 cm, i.e., 0.5% 8m telescope; longitudinal pupil position error 1 m. 3. Wavefront sensing (error 80 nm) So we need a beam analyzing system and correction system!!

Acquisition camera optical layout

Acquisition camera: folding optics UT4 UT3 UT2 UT1

Acquisition camera: core beam analyzer Pupil tracker Aberration sensor Pupil imager Field tracker Optics embedded in it

1. Pupil tracking ü To track telescope pupil motions, 4 lasers are mounted on M2 spiders. ü Lasers are imaged with 2x2 lenslet.

a) Lateral pupil tracking

b) Longitudinal pupil tracking

Pupil shifts measurement Lateral pupil shifts Longitudinal pupil shifts

2. Field imaging and tracking AO residual and tunnel seeing tip-tilts are measured with a precision of 2 milliarcsecond.

Atmospheric dispersion shifts between acquisition camera and K-band fiber

GRAVITY Acquisition camera

Acquisition camera Real Time Display

For one telescope Pupil tracker Aberration sensor Pupil imager Field imager

Software developed Main tasks: 1. Image reduction software 2. Closed loop correction software. 3. Automatic alignment of GRAVITY with the VLTI optics. Image reduction software Instrument Database Closed loop correction software Automatic alignment software

Pupil tracking characterization with calibration unit By applying known pupil shifts the pupil tracker is characterized.

Field tracking characterization Tip-tilts Star magnitude Fiber flux

Aberration sensor characterization By applying known wavefront error the aberration sensor characterized.

On-sky field residuals

On-sky pupil residuals

Further improvements progressing 1. Robust pupil sensor in the presence of background and vignetting. 2. Wavefront sensing in the presence of low SNR and in vignetting cases.

Conclusions Field Tracker: Active in closed loop field stabilization. Pupil Tracker: Active in pupil stabilization. Aberration tracker: Quasi-static higher order wavefront aberrations measurement. Currently they are used for defocus correction. ü Used in automated alignment of GRAVITY with the telescopes. ü The beams guiding satisfies GRAVITY specifications.

Many thanks