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        <identifier>oai:www.ideals.illinois.edu:2142/85071</identifier>
        <datestamp>2023-07-11</datestamp>
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          <dc:contributor>Conway, Bruce A.</dc:contributor>
          <dc:creator>Horie, Kazuhiro</dc:creator>
          <dc:date>2015-09-25T22:34:19Z</dc:date>
          <dc:date>2015-09-25T22:34:19Z</dc:date>
          <dc:date>10000-01-01</dc:date>
          <dc:date>2002</dc:date>
          <dc:date>2002</dc:date>
          <dc:description>This research successfully develops a new numerical method for the problem of two-sided flight path optimization, that is, a method capable of finding trajectories satisfying the necessary condition of an open-loop representation of a saddle-point trajectory. The method of direct collocation with nonlinear programming is extended to find the solution of a zerosum two-person differential game by incorporating the analytical optimality condition for one player into the system equations. The new method is named semi-direct collocation with nonlinear programming (semi-DCNLP). We apply the new method to a variety of problems of increasing complexity; the dolichobrachistochrone, a problem of ballistic interception, the homicidal chauffeur problem and minimum-time spacecraft interception for optimally evasive target, and thus verify that the method is capable of identifying saddle-point trajectories. While the method is quite robust, ambitious problems require a reasonable initial guess of the discretized solution from which the optimizer may converge. A method for generating a good initial guess, requiring no a priori information about the solution, is developed using genetic algorithms. The semi-DCNLP, in combination with the genetic algorithm-based preprocessor, is then used to solve a very complicated pursuit-evasion problem; optimal air combat for realistic fighter aircraft models in three dimensions. Characteristics of the optimal air combat maneuvers for both aircraft are identified for many different initial conditions.</dc:description>
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  Previous issue date: 2002</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 86352
Lift date: Forever
Reason: Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs</dc:description>
          <dc:description>Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs</dc:description>
          <dc:description>U of I Only</dc:description>
          <dc:description>172 p.</dc:description>
          <dc:description>Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2002.</dc:description>
          <dc:identifier>http://hdl.handle.net/2142/85071</dc:identifier>
          <dc:identifier>(MiAaPQ)AAI3044118</dc:identifier>
          <dc:language>eng</dc:language>
          <dc:subject>Engineering, Aerospace</dc:subject>
          <dc:title>Collocation With Nonlinear Programming for Two-Sided Flight Path Optimization</dc:title>
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          <degree>
            <department>Aerospace Engineering</department>
            <discipline>Aerospace Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Dissertation</level>
            <name>Ph.D.</name>
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