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    Path Optimization From En Route 3D-Printed Aircraft Using Physics-Based Estimation Methods and Surrogate Models

    Source: Journal of Mechanical Design:;2026:;volume( 148 ):;issue:004::page 140
    Author:
    Dickerson, Tevin J.
    ,
    Salmon, John L.
    ,
    Mattson, Christopher A.
    DOI: 10.1115/1.4069685
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In a previous study, a general approach to increasing the range capability of an unmanned aerial system was assessed by 3D printing components or parts for the unmanned aerial systems (UAS) while a carrier platform, of both the printer and UAS systems, travels to a launch point for the UAS. As a result, the platform could launch the UAS from a distance further away from the location of interest. This article outlines the parameters of a physics-based model to determine the actual range increase of an attritable aircraft, constrained by the amount of time available for printing while en route. It develops the formulation of the UAS range increase from the lift-to-drag ratio increases caused by the physical wing section enhancements printed in a constrained amount of time while the carrier platform travels from one location to another. The relationship is leveraged to optimize the shortest path necessary for the carrier platform to access or reach the set of locations of interest in an operational environment. Scenarios of up to 15 locations are explored by first optimizing the sequence of the locations in a traveling salesman problem and then optimizing the actual path taken by the carrier platform along that sequence. Statistical results are presented to summarize the benefits of 3D printing en route across different scenarios.
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      Path Optimization From En Route 3D-Printed Aircraft Using Physics-Based Estimation Methods and Surrogate Models

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316680
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    • Journal of Mechanical Design

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    contributor authorDickerson, Tevin J.
    contributor authorSalmon, John L.
    contributor authorMattson, Christopher A.
    date accessioned2026-08-23T08:31:41Z
    date available2026-08-23T08:31:41Z
    date copyright2026/04/01
    date issued2026
    identifier issn1050-0472
    identifier othermd-24-1655.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316680
    description abstractAbstract. In a previous study, a general approach to increasing the range capability of an unmanned aerial system was assessed by 3D printing components or parts for the unmanned aerial systems (UAS) while a carrier platform, of both the printer and UAS systems, travels to a launch point for the UAS. As a result, the platform could launch the UAS from a distance further away from the location of interest. This article outlines the parameters of a physics-based model to determine the actual range increase of an attritable aircraft, constrained by the amount of time available for printing while en route. It develops the formulation of the UAS range increase from the lift-to-drag ratio increases caused by the physical wing section enhancements printed in a constrained amount of time while the carrier platform travels from one location to another. The relationship is leveraged to optimize the shortest path necessary for the carrier platform to access or reach the set of locations of interest in an operational environment. Scenarios of up to 15 locations are explored by first optimizing the sequence of the locations in a traveling salesman problem and then optimizing the actual path taken by the carrier platform along that sequence. Statistical results are presented to summarize the benefits of 3D printing en route across different scenarios.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePath Optimization From En Route 3D-Printed Aircraft Using Physics-Based Estimation Methods and Surrogate Models
    typeJournal Paper
    journal volume148
    journal issue4
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.4069685
    journal fristpage140
    journal lastpage151
    page12
    treeJournal of Mechanical Design:;2026:;volume( 148 ):;issue:004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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