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    Structure/Control Synthesis with Nonnegligible Actuator Mass

    Source: Journal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 001
    Author:
    David C. Zimmerman
    DOI: 10.1061/(ASCE)0893-1321(1993)6:1(76)
    Publisher: American Society of Civil Engineers
    Abstract: Simultaneous design of a structure/active control system in which the mass of the actuators required to implement the active control is considered is addressed. The inclusion of required actuator mass essentially tightens the coupling between structure and control dynamics and introduces an inner iteration loop in the overall design process. Because this inner iteration loop significantly increases the computational burden, an algorithm for estimating the required actuator mass, given the control law and the desired maneuver, is presented. Additionally, a secant‐based actuator mass update algorithm is investigated in order to improve convergence characteristics of the inner iteration loop. A nonlinear optimization algorithm is used to direct the design process. The methodology is demonstrated on the design of a large two‐dimensional L‐shaped structure in which it is desired to minimize the line‐of‐sight‐pointing error between the two ends of the L after a worst‐case slew maneuver.
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      Structure/Control Synthesis with Nonnegligible Actuator Mass

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44760
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    contributor authorDavid C. Zimmerman
    date accessioned2017-05-08T21:15:45Z
    date available2017-05-08T21:15:45Z
    date copyrightJanuary 1993
    date issued1993
    identifier other%28asce%290893-1321%281993%296%3A1%2876%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44760
    description abstractSimultaneous design of a structure/active control system in which the mass of the actuators required to implement the active control is considered is addressed. The inclusion of required actuator mass essentially tightens the coupling between structure and control dynamics and introduces an inner iteration loop in the overall design process. Because this inner iteration loop significantly increases the computational burden, an algorithm for estimating the required actuator mass, given the control law and the desired maneuver, is presented. Additionally, a secant‐based actuator mass update algorithm is investigated in order to improve convergence characteristics of the inner iteration loop. A nonlinear optimization algorithm is used to direct the design process. The methodology is demonstrated on the design of a large two‐dimensional L‐shaped structure in which it is desired to minimize the line‐of‐sight‐pointing error between the two ends of the L after a worst‐case slew maneuver.
    publisherAmerican Society of Civil Engineers
    titleStructure/Control Synthesis with Nonnegligible Actuator Mass
    typeJournal Paper
    journal volume6
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1993)6:1(76)
    treeJournal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 001
    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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