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升级GRAVITY条纹跟踪器以支持GRAVITY+:在不可观测的光程长度状态空间中跟踪白光条纹

Upgrading the GRAVITY fringe tracker for GRAVITY+: Tracking the white light fringe in the non-observable Optical Path Length state-space

M. Nowak, S. Lacour, R. Abuter, J. Woillez, R. Dembet, M. S. Bordoni, G. Bourdarot, B. Courtney-Barrer, D. Defrère, A. Drescher, F. Eisenhauer, M. Fabricius, H.… 展开作者

M. Nowak, S. Lacour, R. Abuter, J. Woillez, R. Dembet, M. S. Bordoni, G. Bourdarot, B. Courtney-Barrer, D. Defrère, A. Drescher, F. Eisenhauer, M. Fabricius, H. Feuchtgruber, R. Frahm, P. Garcia, S. Gillessen, V. Gopinath, J. Graf, S. Hoenig, L. Kreidberg, R. Laugier, J. B. Le Bouquin, D. Lutz, F. Mang, F. Millour, N. More, N. Morujão, T. Ott, T. Paumard, G. Perrin, C. Rau, D. C. Ribeiro, J. Shangguan, T. Shimizu, F. Soulez, C. Straubmeier, F. Widmann, B. Wolff

AI总结:

通过修改群延迟控制器和引入不可观测光程状态空间的卡尔曼滤波跟踪,GRAVITY+条纹跟踪器实现了白光条纹稳定跟踪,相位残差降低30-40%,并支持其他仪器使用。

摘要:

目的:作为甚大望远镜干涉仪基础设施正在进行的GRAVITY+升级的一部分,我们旨在提高GRAVITY条纹跟踪器的性能,并使其能够被其他仪器使用。方法:我们修改了群延迟控制器,以持续维持在白光条纹中的跟踪,该条纹以最小群延迟为特征。此外,我们引入了一种新方法,即在不可观测的光程长度状态空间中进行条纹跟踪,使用协方差加权卡尔曼滤波器和扰动的自回归模型。我们概述了这一新的状态空间表示,以及我们用于传播状态向量和生成控制信号的形式体系。虽然我们的方法是在GRAVITY/GRAVITY+的背景下具体提出的,但它可以很容易地适应其他仪器或干涉测量设施。结果:我们成功地在单个条纹内实现了相位延迟跟踪,任何杂散相位跳变都能在不到100毫秒内被检测并纠正。我们还报告了显著的性能提升,表现为相位残差减少了约30%至40%,并且在次优大气条件下表现更好。与2019年观察到的相比,辅助望远镜上的中位残差从150纳米降低到100纳米,单位望远镜上的中位残差从250纳米降低到150纳米。结论:改进的相位延迟跟踪结合白光条纹跟踪意味着从现在起,GRAVITY条纹跟踪器可以被在不同波段工作的其他仪器使用。唯一的限制仍然是对光程色散调整的需求。

英文摘要:

Aims. As part of the ongoing GRAVITY+ upgrade of the Very Large Telescope Interferometer infrastructure, we aim to improve the performance of the GRAVITY Fringe-Tracker, and to enable its use by other instruments. Methods. We modify the group delay controller to consistently maintain tracking in the white light fringe, characterised by a minimum group delay. Additionally, we introduce a novel approach in which fringe-tracking is performed in the non-observable Optical Path Length state-space, using a covariance-weighted Kalman filter and an auto-regressive model of the disturbance. We outline this new state-space representation, and the formalism we use to propagate the state-vector and generate the control signal. While our approach is presented specifically in the context of GRAVITY/GRAVITY+, it can easily be adapted to other instruments or interferometric facilities. Results. We successfully demonstrate phase delay tracking within a single fringe, with any spurious phase jumps detected and corrected in less than 100 ms. We also report a significant performance improvement, as evidenced by a reduction of about 30 to 40% in phase residuals, and a much better behaviour under sub-optimal atmospheric conditions. Compared to what was observed in 2019, the median residuals have decreased from 150 nm to 100 nm on the Auxiliary Telescopes and from 250 nm to 150 nm on the Unit Telescopes. Conclusions. The improved phase-delay tracking combined with whit light fringe tracking means that from now-on, the GRAVITY Fringe-Tracker can be used by other instruments operating in different wavebands. The only limitation remains the need for an optical path dispersion adjustment.

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