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• W2121054725 abstract "The performance of many spacecraft can be improved by using closed-loop control and command-shaping techniques to reduce problematic vibration. However, due to uncertainties about the operation of controlled structures in zero-gravity, little information exists to give designers confidence in eventual on-orbit performance. The Middeck Active Control Experiment (MACE), scheduled for launch aboard the Space Shuttle Endeavor in March 1995, is designed to investigate these issues by collecting on-orbit data from a controlled flexible structure. In addition to providing a description of the MACE project, this paper presents 0-g predictions for some of the MACE command shaping experiments and describes how the anticipated mission results will be used to understand how to improve the performance of other space systems." @default.
• W2121054725 created "2016-06-24" @default.
• W2121054725 creator A5030177743 @default.
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• W2121054725 date "2005-08-24" @default.
• W2121054725 modified "2023-09-25" @default.
• W2121054725 title "Vibration reduction in 0-g using input shaping on the MIT Middeck Active Control Experiment" @default.
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• W2121054725 doi "https://doi.org/10.1109/acc.1995.529382" @default.
• W2121054725 hasPublicationYear "2005" @default.
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