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dc.contributor.authorFeng, Xiaofanen_US
dc.contributor.authorSchott, Johnen_US
dc.contributor.authorGallagher, Timothyen_US
dc.date.accessioned2007-07-05T13:42:22Zen_US
dc.date.available2007-07-05T13:42:22Zen_US
dc.date.issued1994-04-01en_US
dc.identifier.citationOptical Engineering 33N4 (1994) 1214-1222en_US
dc.identifier.issn0091-3286en_US
dc.identifier.urihttp://hdl.handle.net/1850/4204en_US
dc.descriptionRIT community members may access full-text via RIT Libraries licensed databases: http://library.rit.edu/databases/
dc.description.abstractThe Digital Imaging and Remote Sensing Laboratory at the Rochester Institute of Technology is developing a new airborne multispectral imaging scanner. One of the most critical components of the scanner system is the scan mirror assembly. The scan mirror must satisfy at least two basic requirements: (1) optical image quality: the image blur caused by deformation of the mirror surface should not exceed the detector size, and (2) mechanical stability: the scan mirror assembly must be dynamically balanced to prevent vibration due to centrifugal force. Due to the large size (6-in. diameter) and high rotation speed (4800 rpm), these two requirements are difficult to meet at the same time. We present a modeling approach for evaluation of mechanical design alternatives using image quality metrics. Several mirror design configurations were evaluated. Each configuration was modeled using a finite element analysis method. The deformation of the mirror surface as well as the centrifugal forces were calculated. The image quality was modeled using optical image formation theory. The modeling approach was validated experimentally. A 3-in. scan mirror was modeled using the same procedures, and the line spread function (LSF) of the scan mirror due to the deformation at high speed was calculated. The actual LSF at that speed was also measured using a CCD linear array camera. The test results obtained with a 3-in. mirror agree with the model within 20% in the width of the LSF. (Approximately 500% error is observed if no distortion is assumed.)en_US
dc.description.sponsorshipn/aen_US
dc.language.isoen_USen_US
dc.publisherThe International Society for Optical Engineering (SPIE)en_US
dc.relation.ispartofseriesvol. 33en_US
dc.relation.ispartofseriesno. 4en_US
dc.subjectFinite elementen_US
dc.subjectModulation transfer functionen_US
dc.subjectOptomechanical designen_US
dc.titleModeling the performance of a high-speed scan mirror for an airborne line scanneren_US
dc.typeArticleen_US
dc.identifier.urlhttp://dx.doi.org/10.1117/12.166934


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