YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Safety-Optimal Linearized Impulsive Rendezvous with Trajectory Uncertainties

    Source: Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 006
    Author:
    Ya-zhong Luo
    ,
    Li-bo Liang
    ,
    Zhi-yong Niu
    ,
    Guo-jin Tang
    DOI: 10.1061/(ASCE)AS.1943-5525.0000366
    Publisher: American Society of Civil Engineers
    Abstract: Different from the current studies on the impulsive rendezvous which are mainly normal propellant-optimal or time-optimal designs, the safety-optimal impulsive rendezvous with consideration of practical trajectory uncertainties is investigated in this paper. An optimization model for safety-optimal rendezvous is established based on the Clohessy-Wiltshire (C-W) equations, which employs one new, recently proposed quantitative performance index of the rendezvous trajectory safety as the objective function. A real-coded genetic algorithm is adopted to locate the optimal solution. The safety index and the optimization approach are tested by several rendezvous problems with different numbers of impulses and different approach directions. The practical application value of the safety-optimal rendezvous trajectory is demonstrated by comparing with the traditional propellant-optimal and time-optimal rendezvous trajectories.
    • Download: (10.86Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Safety-Optimal Linearized Impulsive Rendezvous with Trajectory Uncertainties

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/56513
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorYa-zhong Luo
    contributor authorLi-bo Liang
    contributor authorZhi-yong Niu
    contributor authorGuo-jin Tang
    date accessioned2017-05-08T21:34:32Z
    date available2017-05-08T21:34:32Z
    date copyrightNovember 2014
    date issued2014
    identifier other%28asce%29as%2E1943-5525%2E0000369.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56513
    description abstractDifferent from the current studies on the impulsive rendezvous which are mainly normal propellant-optimal or time-optimal designs, the safety-optimal impulsive rendezvous with consideration of practical trajectory uncertainties is investigated in this paper. An optimization model for safety-optimal rendezvous is established based on the Clohessy-Wiltshire (C-W) equations, which employs one new, recently proposed quantitative performance index of the rendezvous trajectory safety as the objective function. A real-coded genetic algorithm is adopted to locate the optimal solution. The safety index and the optimization approach are tested by several rendezvous problems with different numbers of impulses and different approach directions. The practical application value of the safety-optimal rendezvous trajectory is demonstrated by comparing with the traditional propellant-optimal and time-optimal rendezvous trajectories.
    publisherAmerican Society of Civil Engineers
    titleSafety-Optimal Linearized Impulsive Rendezvous with Trajectory Uncertainties
    typeJournal Paper
    journal volume27
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000366
    treeJournal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 006
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian