Model-based optimal control design for the orbit feedback system at the Siam Photon Source

A model-based optimal control approach has been developed for the slow orbit feedback (SOFB) system to enhance orbit stability in the Siam Photon Source (SPS) storage ring. The control strategy utilizes a linear quadratic regulator (LQR) based on a multi-input, multi-output (MIMO) state-space model of the linear SPS storage ring, derived through system identification using MATLAB and SIMULINK. The necessary and sufficient conditions for controllability and boundedness of the dynamic system are established. Experimental simulations were conducted to assess the performance of the LQR controller in a practical SPS storage ring. The results demonstrate that the proposed control method effectively minimizes the quadratic cost function and error signals between setpoints and process variables for both horizontal and vertical orbit positions while ensuring system stability and robustness. The study also outlines the fundamental principles of optimal control theory, system identification, and future development directions.

Authors

Publication Details

Journal
JACOW
Published
2026-01-20
DOI
https://doi.org/10.18429/jacow-ibic2025-tupmo27
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Model-based optimal control design for the orbit feedback system at the Siam Photon Source

Natthawut Suradet, Supat Klinkhieo, Somjai Chunjarean, Nattawat Yachum et al.
JACOW
Spacecraft Dynamics and Control
article

Model-based optimal control design for the orbit feedback system at the Siam Photon Source

Natthawut Suradet, Supat Klinkhieo, Somjai Chunjarean, Nattawat Yachum, Thakonwat Chanwattana, Thapakron Pulampong, Surapong Kokkrathoke
article en

Abstract

A model-based optimal control approach has been developed for the slow orbit feedback (SOFB) system to enhance orbit stability in the Siam Photon Source (SPS) storage ring. The control strategy utilizes a linear quadratic regulator (LQR) based on a multi-input, multi-output (MIMO) state-space model of the linear SPS storage ring, derived through system identification using MATLAB and SIMULINK. The necessary and sufficient conditions for controllability and boundedness of the dynamic system are established. Experimental simulations were conducted to assess the performance of the LQR controller in a practical SPS storage ring. The results demonstrate that the proposed control method effectively minimizes the quadratic cost function and error signals between setpoints and process variables for both horizontal and vertical orbit positions while ensuring system stability and robustness. The study also outlines the fundamental principles of optimal control theory, system identification, and future development directions.

JACOW
Openalex Percentile: Top 85%
Spacecraft Dynamics and Control
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