Closed-loop correction for slow-varying tracking error at the AIMS Coudé Focal Plane

The Accurate Infrared Magnetic Field Measurements of the Sun (AIMS) project requires a root-mean-square tracking accuracy of 1″/30min to observe targets on the solar disk. Since the terminal scientific instruments in AIMS are positioned at the Coudé focus, the telescope and guiding optical path introduce slowly varying nonlinear tracking errors during solar tracking, which degrade long-duration tracking accuracy. To address this issue, we first analyze the mechanisms and characteristics of these slowly varying tracking errors at the Coudé focus, based on the optical-mechanical structure of AIMS and motion principles, and conduct actual measurements of the tracking errors. We have designed a closed-loop correction scheme in conjunction with the optical-mechanical mechanisms of AIMS, detailing both hardware and software implementations. Following over a year of testing and trial use on AIMS, results demonstrate that the system can stably perform closed-loop tracking of solar observation targets for over 30 minutes, with a tracking error of less than 1.0″. Both the tracking duration and error value meet tracking accuracy requirements.

Authors

Publication Details

Journal
Astronomical Techniques and Instrument
Published
2025-10-01
DOI
https://doi.org/10.3724/ati2025062
Primary Topic
Solar and Space Plasma Dynamics
Type
article
Field-Weighted Citation Impact
0.00

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Closed-loop correction for slow-varying tracking error at the AIMS Coudé Focal Plane

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Astronomical Techniques and Instrument
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Closed-loop correction for slow-varying tracking error at the AIMS Coudé Focal Plane

Guangqian Liu, Hengyu Mu, Songbo Xu, Yuliang Shen, Dongguang Wang, Zhijie Shi
article en

Abstract

The Accurate Infrared Magnetic Field Measurements of the Sun (AIMS) project requires a root-mean-square tracking accuracy of 1″/30min to observe targets on the solar disk. Since the terminal scientific instruments in AIMS are positioned at the Coudé focus, the telescope and guiding optical path introduce slowly varying nonlinear tracking errors during solar tracking, which degrade long-duration tracking accuracy. To address this issue, we first analyze the mechanisms and characteristics of these slowly varying tracking errors at the Coudé focus, based on the optical-mechanical structure of AIMS and motion principles, and conduct actual measurements of the tracking errors. We have designed a closed-loop correction scheme in conjunction with the optical-mechanical mechanisms of AIMS, detailing both hardware and software implementations. Following over a year of testing and trial use on AIMS, results demonstrate that the system can stably perform closed-loop tracking of solar observation targets for over 30 minutes, with a tracking error of less than 1.0″. Both the tracking duration and error value meet tracking accuracy requirements.

Astronomical Techniques and Instrument
National Natural Science Foundation of China
Openalex Percentile: Top 23%
Solar and Space Plasma Dynamics
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