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GUO Ming, FAN Yi-di, WANG Peng-cheng, AN Ke, LU Wei, CHEN Wen, ZHANG Yong-he, LIN Bao-jun. High-precision beam pointing control based on global non-singular attitude estimation[J]. Chinese Optics. doi: 10.37188/CO.EN-2026-0004
Citation: GUO Ming, FAN Yi-di, WANG Peng-cheng, AN Ke, LU Wei, CHEN Wen, ZHANG Yong-he, LIN Bao-jun. High-precision beam pointing control based on global non-singular attitude estimation[J]. Chinese Optics. doi: 10.37188/CO.EN-2026-0004

High-precision beam pointing control based on global non-singular attitude estimation

cstr: 32171.14.CO.EN-2026-0004
Funds:  This work was supported by National Key R&D Program of China (No. 2022YFC2203700, No. 2021YFC2202600,) and the Shanghai Science and Technology Innovation Action Plan (No. 24YF2742600).
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  • Author Bio:

    GUO Ming (1991—), male, born in Laiwu, Shandong Province. Ph.D. candidate at the Innovation Academy for Microsatellites, Chinese Academy of Sciences, his research mainly focuses on spacecraft system design. Email: guom@microsate.com

    FAN Yi-di (1993–), female, born in Lianyungang, Jiangsu Province. She received her Ph.D. from the Harbin Institute of Technology and is now an assistant research fellow. Her research focuses on spacecraft dynamics and control. Email: fanyd@microsate.com

  • Corresponding author: fanyd@microsate.com
  • Received Date: 08 Jan 2026
  • Accepted Date: 05 Mar 2026
  • Available Online: 07 Aug 2026
  • Focusing on the key problem of establishing inter-spacecraft laser links for space-borne gravitational wave (GW) detection, this paper presents a high-precision beam pointing control scheme founded on multi-source information fusion. A detailed state-space model is constructed by integrating the coupled dynamics of moving optical sub-assemblies. Using error quaternions, the nonlinear measurement equations are linearized, thereby enhancing the accuracy of filter-based attitude determination via inertial sensor fusion. Furthermore, a time-varying analytical formulation of the point-ahead angle (PAA) is derived, supplying a theoretical basis for servo compensation. Closed-loop simulations of a three-spacecraft configuration validate the stability and accuracy of the proposed estimation algorithm. In combination with robust disturbance-rejection control, the method enables highly accurate beam pointing, providing essential technical support for GW detection missions.

     

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