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    Optimization of Step Rockets by the Discrete Maximum Principle

    Source: Journal of Manufacturing Science and Engineering:;1965:;volume( 087 ):;issue: 004::page 419
    Author:
    Liang-Tseng Fan
    ,
    Ching-Lai Hwang
    ,
    Chiu-Sen Wang
    DOI: 10.1115/1.3670855
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The general algorithm of the discrete maximum principle with information feedback is stated briefly. It is applied to obtain solutions for the optimum stage-weight distribution problems of a multistage rocket vehicle. The first problem treats the structure ratio as a constant in each stage, though it may differ stage by stage. The second problem considers the variations in structural factors with stage weight. The third problem obtains the optimum weight distribution which minimizes hardware weight. Specific examples are solved.
    keyword(s): Optimization , Rockets , Weight (Mass) , Hardware , Algorithms , Vehicles AND Feedback ,
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      Optimization of Step Rockets by the Discrete Maximum Principle

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/108523
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    contributor authorLiang-Tseng Fan
    contributor authorChing-Lai Hwang
    contributor authorChiu-Sen Wang
    date accessioned2017-05-08T23:35:29Z
    date available2017-05-08T23:35:29Z
    date copyrightNovember, 1965
    date issued1965
    identifier issn1087-1357
    identifier otherJMSEFK-27495#419_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108523
    description abstractThe general algorithm of the discrete maximum principle with information feedback is stated briefly. It is applied to obtain solutions for the optimum stage-weight distribution problems of a multistage rocket vehicle. The first problem treats the structure ratio as a constant in each stage, though it may differ stage by stage. The second problem considers the variations in structural factors with stage weight. The third problem obtains the optimum weight distribution which minimizes hardware weight. Specific examples are solved.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimization of Step Rockets by the Discrete Maximum Principle
    typeJournal Paper
    journal volume87
    journal issue4
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3670855
    journal fristpage419
    journal lastpage424
    identifier eissn1528-8935
    keywordsOptimization
    keywordsRockets
    keywordsWeight (Mass)
    keywordsHardware
    keywordsAlgorithms
    keywordsVehicles AND Feedback
    treeJournal of Manufacturing Science and Engineering:;1965:;volume( 087 ):;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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