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    String Instabilities in Formation Flight: Limitations Due to Integral Constraints

    Source: Journal of Dynamic Systems, Measurement, and Control:;2004:;volume( 126 ):;issue: 004::page 873
    Author:
    P. Seiler
    ,
    A. Pant
    ,
    J. K. Hedrick
    DOI: 10.1115/1.1858444
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flying in formation improves aerodynamic efficiency and, consequently, leads to an energy savings. One strategy for formation control is to follow the preceding vehicle. Many researchers have shown through simulation results and analysis of specific control laws that this strategy leads to amplification of disturbances as they propagate through the formation. This effect is known as string instability. In this paper, we show that string instability is due to a fundamental constraint on coupled feedback loops. The tradeoffs imposed by this constraint imply that predecessor following is an inherently poor strategy for formation flight control. Finally, we present two examples that demonstrate the theoretical results.
    keyword(s): String , Vehicles , Errors , Feedback , Flight , Dynamics (Mechanics) , Aircraft , Transfer functions , Control equipment AND Helicopters ,
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      String Instabilities in Formation Flight: Limitations Due to Integral Constraints

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/129727
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorP. Seiler
    contributor authorA. Pant
    contributor authorJ. K. Hedrick
    date accessioned2017-05-09T00:12:29Z
    date available2017-05-09T00:12:29Z
    date copyrightDecember, 2004
    date issued2004
    identifier issn0022-0434
    identifier otherJDSMAA-26336#873_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129727
    description abstractFlying in formation improves aerodynamic efficiency and, consequently, leads to an energy savings. One strategy for formation control is to follow the preceding vehicle. Many researchers have shown through simulation results and analysis of specific control laws that this strategy leads to amplification of disturbances as they propagate through the formation. This effect is known as string instability. In this paper, we show that string instability is due to a fundamental constraint on coupled feedback loops. The tradeoffs imposed by this constraint imply that predecessor following is an inherently poor strategy for formation flight control. Finally, we present two examples that demonstrate the theoretical results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleString Instabilities in Formation Flight: Limitations Due to Integral Constraints
    typeJournal Paper
    journal volume126
    journal issue4
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.1858444
    journal fristpage873
    journal lastpage879
    identifier eissn1528-9028
    keywordsString
    keywordsVehicles
    keywordsErrors
    keywordsFeedback
    keywordsFlight
    keywordsDynamics (Mechanics)
    keywordsAircraft
    keywordsTransfer functions
    keywordsControl equipment AND Helicopters
    treeJournal of Dynamic Systems, Measurement, and Control:;2004:;volume( 126 ):;issue: 004
    contenttypeFulltext
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    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