2000
DOI: 10.1143/jjap.39.6094
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A Simulation Study of the Global Orbit Feedback System for Pohang Light Source

Abstract: This paper describes the simulation of the global orbit feedback system using the singular value decomposition (SVD) method, the error minimization method, and the neural network method. Instead of facing unacceptable correction result raised occasionally in the SVD method, we choose the error minimization method for the global orbit feedback. This method provides minimum orbit errors while avoiding unacceptable corrections, and keeps the orbit within the dynamic aperture of the storage ring. We simulate the P… Show more

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Cited by 6 publications
(3 citation statements)
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“…In the early 1990s, scientists at Los Alamos National Lab had some experimental success with neural-network-based ion source control [34][35][36]. Other early studies at the University of New Mexico focused on orbit/trajectory control [37][38][39][40][41], fault detection and management [42,43], and root-cause analysis of errors (e.g. distinguishing between bending magnet misalignment and field defects [44]).…”
Section: Early History Of Usage For Particle Acceleratorsmentioning
confidence: 99%
“…In the early 1990s, scientists at Los Alamos National Lab had some experimental success with neural-network-based ion source control [34][35][36]. Other early studies at the University of New Mexico focused on orbit/trajectory control [37][38][39][40][41], fault detection and management [42,43], and root-cause analysis of errors (e.g. distinguishing between bending magnet misalignment and field defects [44]).…”
Section: Early History Of Usage For Particle Acceleratorsmentioning
confidence: 99%
“…During the 1990s to mid-2000s, NNs in particular were investigated for orbit/trajectory control [68,69,70,71,72], with mixed results. Also during this time, a NN was successfully implemented to detect faulty beamline and diagnostic components [73].…”
Section: ) Previous Efforts To Apply Neural Network To Particle Accmentioning
confidence: 99%
“…In order to quantify the result of the orbit correction, we define the rms reduction rate as the ratio of the rms orbit distortion before and after the correction [4]. In this definition, we exclude the orbit distortion in the constraint region because our aim is to preserve the orbit in the constraint region.…”
Section: Choice Of Bpms and Correctorsmentioning
confidence: 99%