A systematic approach to determining the minimum sampling rate for real-time spacecraft control
dc.contributor.author | Zappulla, Richard II | |
dc.contributor.author | Romano, Marcello | |
dc.date | February 2017 | |
dc.date.accessioned | 2017-03-02T00:03:24Z | |
dc.date.available | 2017-03-02T00:03:24Z | |
dc.date.issued | 2017-02 | |
dc.identifier.other | AAS 17-424 | |
dc.identifier.uri | http://hdl.handle.net/10945/51982 | |
dc.description | To be published in the proceedings of the 27th AAS/AIAA Spaceflight Mechanics Meeting, San Antonio, TX, Feb. 6-9, 2017 | en_US |
dc.description.abstract | Typical 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.rights | This 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.title | A systematic approach to determining the minimum sampling rate for real-time spacecraft control | en_US |
dc.type | Conference Paper | |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
dc.contributor.department | Mechanical and Aerospace Engineering |