Comparison of fringe-tracking algorithms for single-mode near-infrared long-baseline interferometers

被引:14
作者
Choquet, E. [1 ,2 ,3 ,4 ]
Menu, J. [5 ]
Perrin, G. [1 ,2 ,3 ]
Cassaing, F. [2 ,3 ,6 ]
Lacour, S. [1 ,2 ,3 ]
Eisenhauer, F. [7 ]
机构
[1] Paris Sci & Lettres Res Univ, Univ Paris Diderot, Observ Paris, LESIA,CNRS,UPMC, F-92195 Meudon, France
[2] CNRS, Observ Paris, ONERA, Grp Interet Sci PHASE Partenariat Haute Resolut A, F-75700 Paris, France
[3] Univ Paris Diderot, Paris, France
[4] Space Telescope Sci Inst, Baltimore, MD 21218 USA
[5] Katholieke Univ Leuven, Inst Sterrenkunde, B-3001 Leuven, Belgium
[6] Off Natl Etud & Rech Aerosp, F-92322 Chatillon, France
[7] Max Planck Inst Extraterr Phys, D-85741 Garching, Germany
来源
ASTRONOMY & ASTROPHYSICS | 2014年 / 569卷
关键词
instrumentation: high angular resolution; atmospheric effects; methods: numerical; techniques: interferometric; FRONT OUTER SCALE; WAVE; INSTRUMENT;
D O I
10.1051/0004-6361/201220223
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
To enable optical long baseline interferometry toward faint objects, long integrations are necessary despite atmospheric turbulence. Fringe trackers are needed to stabilize the fringes and thus increase the fringe visibility and phase signal-to-noise ratio (S/N), with efficient controllers robust to instrumental vibrations and to subsequent path fluctuations and flux drop-outs. We report on simulations, analysis, and comparison of the performances of a classical integrator controller and of a Kalman controller, both optimized to track fringes under realistic observing conditions for different source magnitudes, disturbance conditions, and sampling frequencies. The key parameters of our simulations (instrument photometric performance, detection noise, turbulence, and vibrations statistics) are based on typical observing conditions at the Very Large Telescope observatory and on the design of the GRAVITY instrument, a 4-telescope single-mode long-baseline interferometer in the near-infrared, next in line to be installed at VLT Interferometer. We find that both controller performances follow a two-regime law with the star magnitude, a constant disturbance limited regime, and a diverging regime limited by both the detector and photon-noise. Moreover, we find that the Kalman controller is optimal in the high and medium S/N regime owing to its predictive commands based on an accurate disturbance model. In the low S/N regime, the model is not accurate enough to be more robust than an integrator controller. Identifying the disturbances from high S/N measurements improves the Kalman performances in the case of strong optical path difference disturbances.
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页数:17
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