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        <datestamp>2023-07-11</datestamp>
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        <thesis xmlns="http://www.ndltd.org/standards/metadata/etdms/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/" xsi:schemaLocation="http://www.ndltd.org/standards/metadata/etdms/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdms11.xsd http://purl.org/dc/elements/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdmsdc.xsd">
          <dc:contributor>Bretl, Timothy</dc:contributor>
          <dc:creator>Figueroa, Felipe</dc:creator>
          <dc:date>2019-08-23T20:05:24Z</dc:date>
          <dc:date>2019-08-23T20:05:24Z</dc:date>
          <dc:date>2019-04-26</dc:date>
          <dc:date>2019-05</dc:date>
          <dc:description>In this thesis we describe the design, manufacturing, and testing of a dynamically scaled aircraft, which is a scaled model of a general aviation vehicle that dynamically behaves in a similar manner as the full-scale aircraft. This scaled model (Cirrus SR22T) is to serve as a testbed for both Distributed Electric Propulsion (DEP) aircraft research and for Visual Inertial Odometry (VIO) research. The aircraft is used as a baseline to compare with the DEP aircraft, to draw conclusion regarding the effect of changing to a DEP configuration, and to provide a way to measure the effect that a DEP configuration would have on a full-scale aircraft. The aircraft is also used to collect data from various onboard sensors to provide a data set for the VIO research community to use.</dc:description>
          <dc:description>Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2019-08-22 without embargo terms</dc:description>
          <dc:description>The student, Felipe Figueroa, accepted the attached license on 2019-04-26 at 10:52.</dc:description>
          <dc:description>The student, Felipe Figueroa, submitted this Thesis for approval on 2019-04-26 at 10:57.</dc:description>
          <dc:description>This Thesis was approved for publication on 2019-04-26 at 15:01.</dc:description>
          <dc:description>DSpace SAF Submission Ingestion Package generated from Vireo submission #13943 on 2019-08-22 at 14:47:06</dc:description>
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  Previous issue date: 2019-04-26</dc:description>
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          <dc:identifier>http://hdl.handle.net/2142/104948</dc:identifier>
          <dc:language>en</dc:language>
          <dc:rights>Copyright 2019 Felipe Figueroa</dc:rights>
          <dc:subject>Distributed Electric Propulsion, DEP, Dynamically Scaled, UAV, Visual Inertia Odometry, VIO, Dataset, Model, System Identification, Parameter Estimation</dc:subject>
          <dc:title>Development and evaluation of a dynamically scaled testbed aircraft for a visual inertial odometry dataset</dc:title>
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            <department>Aerospace Engineering</department>
            <discipline>Aerospace Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Thesis</level>
            <name>M.S.</name>
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