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Distributed Optimization Method for Spacecraft Attitude Control and Vibration Suppression

  • Harbin Institute of Technology
  • Polytechnic University of Milan

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)752-760
Number of pages9
JournalJournal of Guidance, Control, and Dynamics
Volume46
Issue number4
DOIs
StatePublished - Apr 2023

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