2023
DOI: 10.1109/taes.2023.3257777
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Interval Uncertainty-Oriented Optimal Control Method for Spacecraft Attitude Control

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Cited by 27 publications
(11 citation statements)
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References 34 publications
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“…The experimental values of deflection achieved by NIST, and measured with sensors [47,48], are very similar to the numerical results, although at the right end of the bridge main support there is a small divergence.…”
Section: Deflection Analysissupporting
confidence: 77%
“…The experimental values of deflection achieved by NIST, and measured with sensors [47,48], are very similar to the numerical results, although at the right end of the bridge main support there is a small divergence.…”
Section: Deflection Analysissupporting
confidence: 77%
“…When considering the robustness of the method used to establish a tool twin model, factors such as model sensitivity and accuracy play a vital role [27,28]. The accuracy value is calculated by comparing the actual and the predicted results.…”
Section: Resultsmentioning
confidence: 99%
“…The waveform and spectrum of the impact elastic wave are analyzed to determine the location, size and boundary of the defect [55,56]. In recent years, due to the rapid development of machine learning, many scholars have used machine learning to optimize the impact-echo method [57,58]. Chen et al [59] carried out the void detection test on a CFST based on the impact-echo method.…”
Section: Void Monitoringmentioning
confidence: 99%