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dc.contributor.authorZappulla, Richard II
dc.contributor.authorRomano, Marcello
dc.dateFebruary 2017
dc.date.accessioned2017-03-02T00:03:24Z
dc.date.available2017-03-02T00:03:24Z
dc.date.issued2017-02
dc.identifier.otherAAS 17-424
dc.identifier.urihttp://hdl.handle.net/10945/51982
dc.descriptionTo be published in the proceedings of the 27th AAS/AIAA Spaceflight Mechanics Meeting, San Antonio, TX, Feb. 6-9, 2017en_US
dc.description.abstractTypical controller design and analysis methods utilize techniques for continuous- time systems. However, digital computation is the favored approach to implement- ing the resulting controllers. This leads to the natural question of choosing an ap- propriate sampling rate for the controller. There exist several ”Rules of Thumbs” for choosing a sample rate derived from primarily frequency domain properties of the system. A metric to estimate the sample rate based on the system properties rooted from first principles is developed. It is then validated via several case stud- ies using representative mechanical systems, actuators, and controllers. Lastly, the paper concludes with a discussion on the applications of this metric.
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleA systematic approach to determining the minimum sampling rate for real-time spacecraft controlen_US
dc.typeConference Paper
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentMechanical and Aerospace Engineering


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