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        <identifier>oai:www.ideals.illinois.edu:2142/22283</identifier>
        <datestamp>2023-07-10</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>Conway, Bruce A.</dc:contributor>
          <dc:creator>Mirfakhraie, Koorosh</dc:creator>
          <dc:date>2011-05-07T13:34:56Z</dc:date>
          <dc:date>2011-05-07T13:34:56Z</dc:date>
          <dc:date>10000-01-01</dc:date>
          <dc:date>1991</dc:date>
          <dc:description>A method has been developed for determining optimal, i.e. minimum fuel, trajectories for the fixed-time cooperative rendezvous of two spacecraft. The method assumes that the vehicles perform a minimum of three impulsive maneuvers with each vehicle being active, that is, making at least one maneuver. The cost of a reference rendezvous solution is improved by an optimizer which uses an analytical gradient developed using primer vector theory and a new solution for the optimal terminal (rendezvous) maneuver. Results are presented for a large number of cases in which the allotted time for rendezvous and other problem parameters including initial relative position, engine efficiencies, initial masses, and fuel mass fractions of the two vehicles are varied. Further improvement in cost may be realized when an additional, i.e. mid-course, impulse is allowed as part of one of the vehicles' trajectory. The criteria for addition of a mid-course impulse to a neighboring solution trajectory has been developed. The cooperative rendezvous proves advantageous particularly in missions with relatively short durations and when fuel constraints are present.</dc:description>
          <dc:description>Made available in DSpace on 2011-05-07T13:34:56Z (GMT). No. of bitstreams: 2
license.txt: 4922 bytes, checksum: 910b249b4beec47e7ab768910c8f966f (MD5)
9124462.pdf: 3277382 bytes, checksum: 81bb887087e9d639285fe1956ab9828f (MD5)
  Previous issue date: 1991</dc:description>
          <dc:description>Item marked as restricted to the 'UIUC Users [automated]' Group (id=2) by Howard Ding (hding2@illinois.edu) on 2011-05-07T14:56:34Z
Item is restricted indefinitely.</dc:description>
          <dc:description>Restriction data tranferred 2014-07-01T11:26:27-05:00
Original Data
Group with Access UIUC Users [automated]
Release Date: none
Reason: ETDs are only available to UIUC Users without author permission</dc:description>
          <dc:description>ETDs are only available to UIUC Users without author permission</dc:description>
          <dc:description>U of I Only</dc:description>
          <dc:identifier>AAI9124462</dc:identifier>
          <dc:identifier>(UMI)AAI9124462</dc:identifier>
          <dc:identifier>http://hdl.handle.net/2142/22283</dc:identifier>
          <dc:language>eng</dc:language>
          <dc:rights>Copyright 1991 Mirfakhraie, Koorosh</dc:rights>
          <dc:subject>Engineering, Aerospace</dc:subject>
          <dc:title>Optimal cooperative time-fixed impulsive rendezvous</dc:title>
          <dc:type>text</dc:type>
          <degree>
            <department>Aerospace Engineering</department>
            <discipline>Aerospace Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Dissertation</level>
            <name>Ph.D.</name>
          </degree>
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