Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones
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Publication:1778637
DOI10.1023/A:1015117912846zbMath1116.93360OpenAlexW64577704MaRDI QIDQ1778637
Yu. I. Krylov, S. V. Matsykin, A. S. Buryĭ
Publication date: 17 June 2005
Published in: Automation and Remote Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1023/a:1015117912846
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