YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    Search 
    •   YE&T Library
    • Search
    •   YE&T Library
    • Search
    • 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.

    Search

    Show Advanced FiltersHide Advanced Filters

    Filters

    Use filters to refine the search results.

    Now showing items 1-5 of 5

    • Relevance
    • Title Asc
    • Title Desc
    • Year Asc
    • Year Desc
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100
  • Export
    • CSV
    • RIS
    • Sort Options:
    • Relevance
    • Title Asc
    • Title Desc
    • Issue Date Asc
    • Issue Date Desc
    • Results Per Page:
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100

    Trajectory Analysis for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle’s Upper Stage 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 001
    Author(s): Yunjun Xu
    Publisher: American Society of Civil Engineers
    Abstract: Reusable launch vehicles are a promising business for the future because of their flexibility, reliability, low cost, and good operability. There are two takeoff styles: the vertical takeoff and the horizontal takeoff. ...
    Request PDF

    Real-Time Optimal Coherent Phantom Track Generation via the Virtual Motion Camouflage Approach 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2011:;volume( 133 ):;issue: 005:;page 51005
    Author(s): Yunjun Xu; Gareth Basset
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Coherent phantom track generation through controlling a group of electronic combat air vehicles is currently an area of great interest to the defense agency for the purpose of deceiving a radar ...
    Request PDF

    Robust Stationkeeping Control for Libration Point Quasi-Periodic Orbits 

    Source: Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 002
    Author(s): Yunjun Xu; Shankar Suman
    Publisher: American Society of Civil Engineers
    Abstract: Libration orbit stationkeeping controls are designed based on selected reference quasi-periodic orbit trajectories. The baseline trajectory is designed to meet science requirements and in the same time achieve minimum fuel ...
    Request PDF

    Trajectory Control of Miniature Helicopters Using a Unified Nonlinear Optimal Control Technique 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2011:;volume( 133 ):;issue: 006:;page 61001
    Author(s): Ming Xin; Yunjun Xu; Ricky Hopkins
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is always a challenge to design a real-time optimal full flight envelope controller for a miniature helicopter due to the nonlinear, underactuated, uncertain, and highly coupled nature of ...
    Request PDF

    μ Control for Satellites Formation Flying 

    Source: Journal of Aerospace Engineering:;2007:;Volume ( 020 ):;issue: 001
    Author(s): Yunjun Xu; Norman Fitz-Coy; Rick Lind; Andrew Tatsch
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a
    Request PDF
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     

    Author

    Publisher

    Year

    Type

    Content Type

    Publication Title

    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian