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    Composite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 004::page 04021028-1
    Author:
    Qibao Jin
    ,
    Jianping Yuan
    ,
    Yinghua Li
    DOI: 10.1061/(ASCE)AS.1943-5525.0001256
    Publisher: ASCE
    Abstract: This paper presents a composite control approach that facilitates both stable attitude tracking and vibration suppression of a space flexible slewing truss. An improved proportional-differential (PD) master controller was developed to track the desired slewing trajectory by adopting state feedback methods, which is more stabile than the traditional PD controller; an auxiliary controller based on linear modal observing is proposed to dissipate the vibration energy of the flexible truss. With the improved composite control scheme, the performance of the attitude tracking greatly improved in both response time and convergence character. An adaptive back-stepping controller was designed to guarantee the precision of synchronization precession of dual driving gyro. Simulation results demonstrated the validity of the composite control strategy.
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      Composite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4271359
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    contributor authorQibao Jin
    contributor authorJianping Yuan
    contributor authorYinghua Li
    date accessioned2022-02-01T00:23:16Z
    date available2022-02-01T00:23:16Z
    date issued7/1/2021
    identifier other%28ASCE%29AS.1943-5525.0001256.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4271359
    description abstractThis paper presents a composite control approach that facilitates both stable attitude tracking and vibration suppression of a space flexible slewing truss. An improved proportional-differential (PD) master controller was developed to track the desired slewing trajectory by adopting state feedback methods, which is more stabile than the traditional PD controller; an auxiliary controller based on linear modal observing is proposed to dissipate the vibration energy of the flexible truss. With the improved composite control scheme, the performance of the attitude tracking greatly improved in both response time and convergence character. An adaptive back-stepping controller was designed to guarantee the precision of synchronization precession of dual driving gyro. Simulation results demonstrated the validity of the composite control strategy.
    publisherASCE
    titleComposite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System
    typeJournal Paper
    journal volume34
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001256
    journal fristpage04021028-1
    journal lastpage04021028-8
    page8
    treeJournal of Aerospace Engineering:;2021:;Volume ( 034 ):;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
    yabeshDSpacePersian