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    Sliding Mode Lateral Guidance and Control of Finless Airship

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 035 ):;issue: 002::page 04021131
    Author:
    Amir Saeed
    ,
    Yang Liu
    ,
    M. Zamurad Shah
    ,
    Lei Wang
    ,
    Qing-Guo Wang
    DOI: 10.1061/(ASCE)AS.1943-5525.0001384
    Publisher: ASCE
    Abstract: The path following a finless airship is presented in this paper using a nonunified sliding mode-based lateral guidance and control framework. The outer-guidance loop relies on the airship’s kinematics, and the designed sliding surface is based on the leading angle that generates the heading angle reference commands. For the inner-control loop, the sliding surface is designed based on the yaw error angle generating commands by actuating the propulsion arms. The effectiveness of the proposed framework is validated by using a high-fidelity nonlinear simulation along with actuator dynamics and sensor models having measurement noises and external disturbances. The results demonstrate the effectiveness of the proposed design framework compared to the classical techniques using proportional navigation in the outer-guidance loop and a linear quadratic regulator in the inner-control loop.
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      Sliding Mode Lateral Guidance and Control of Finless Airship

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4283369
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    contributor authorAmir Saeed
    contributor authorYang Liu
    contributor authorM. Zamurad Shah
    contributor authorLei Wang
    contributor authorQing-Guo Wang
    date accessioned2022-05-07T21:08:23Z
    date available2022-05-07T21:08:23Z
    date issued2021-11-27
    identifier other(ASCE)AS.1943-5525.0001384.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4283369
    description abstractThe path following a finless airship is presented in this paper using a nonunified sliding mode-based lateral guidance and control framework. The outer-guidance loop relies on the airship’s kinematics, and the designed sliding surface is based on the leading angle that generates the heading angle reference commands. For the inner-control loop, the sliding surface is designed based on the yaw error angle generating commands by actuating the propulsion arms. The effectiveness of the proposed framework is validated by using a high-fidelity nonlinear simulation along with actuator dynamics and sensor models having measurement noises and external disturbances. The results demonstrate the effectiveness of the proposed design framework compared to the classical techniques using proportional navigation in the outer-guidance loop and a linear quadratic regulator in the inner-control loop.
    publisherASCE
    titleSliding Mode Lateral Guidance and Control of Finless Airship
    typeJournal Paper
    journal volume35
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001384
    journal fristpage04021131
    journal lastpage04021131-12
    page12
    treeJournal of Aerospace Engineering:;2021:;Volume ( 035 ):;issue: 002
    contenttypeFulltext
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    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