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    Intelligent Dynamic Force Loading Algorithm for Aerospace Rudder Load Simulator

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005::page 04023060-1
    Author:
    Jing Huang
    ,
    Cheng Qiu
    ,
    Yanhui You
    ,
    Hong Li
    DOI: 10.1061/JAEEEZ.ASENG-4466
    Publisher: ASCE
    Abstract: In aerospace load simulation loading systems, due to the coupling between the loading system and the system under testing, surplus forces and poor loading accuracies remain to be key issues. To solve this, this paper introduces a new intelligent dynamic force loading algorithm. First, based on the mechanical geometry and fluid theory of the system, a nonlinear mathematical model that can describe the system more accurately is established. By combining the mechanical structure and mathematical model of the system, it is found that the surplus force caused by external disturbances has the greatest impact on the force loading accuracy. The causes of the surplus force are then analyzed and the solutions provided. To improve the force loading performance and eliminate excess force on the controller, an intelligent dynamic force loading algorithm is proposed. This new control algorithm ensures that the surplus force caused by an external disturbance can be suppressed to within the required range in a short time as well as improve the controller performance and dynamic force loading accuracy of the system. Finally, the algorithm is applied to an aerospace air rudder load simulator and its performance is compared with the three other classical control algorithms. The results show that the proposed intelligent control algorithm can attain better accuracy in dynamic force loadings and can attain a control accuracy that meets technical requirements. The load simulator and digital controller involved in this paper are applied in a Chinese Aerospace Research Institute. The load simulator is currently used for testing and product acceptance of the institute’s servo products. Because the control algorithm proposed in this paper meets the requirements of technical indicators and product performance testing requirements, it has been recognized by the institute and has been put into practical use. The technical experts of the institute have verified the experimental results and believe that its control accuracy and loading performance are better than those of the original old load simulator.
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      Intelligent Dynamic Force Loading Algorithm for Aerospace Rudder Load Simulator

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4293243
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    contributor authorJing Huang
    contributor authorCheng Qiu
    contributor authorYanhui You
    contributor authorHong Li
    date accessioned2023-11-27T23:02:47Z
    date available2023-11-27T23:02:47Z
    date issued7/11/2023 12:00:00 AM
    date issued2023-07-11
    identifier otherJAEEEZ.ASENG-4466.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4293243
    description abstractIn aerospace load simulation loading systems, due to the coupling between the loading system and the system under testing, surplus forces and poor loading accuracies remain to be key issues. To solve this, this paper introduces a new intelligent dynamic force loading algorithm. First, based on the mechanical geometry and fluid theory of the system, a nonlinear mathematical model that can describe the system more accurately is established. By combining the mechanical structure and mathematical model of the system, it is found that the surplus force caused by external disturbances has the greatest impact on the force loading accuracy. The causes of the surplus force are then analyzed and the solutions provided. To improve the force loading performance and eliminate excess force on the controller, an intelligent dynamic force loading algorithm is proposed. This new control algorithm ensures that the surplus force caused by an external disturbance can be suppressed to within the required range in a short time as well as improve the controller performance and dynamic force loading accuracy of the system. Finally, the algorithm is applied to an aerospace air rudder load simulator and its performance is compared with the three other classical control algorithms. The results show that the proposed intelligent control algorithm can attain better accuracy in dynamic force loadings and can attain a control accuracy that meets technical requirements. The load simulator and digital controller involved in this paper are applied in a Chinese Aerospace Research Institute. The load simulator is currently used for testing and product acceptance of the institute’s servo products. Because the control algorithm proposed in this paper meets the requirements of technical indicators and product performance testing requirements, it has been recognized by the institute and has been put into practical use. The technical experts of the institute have verified the experimental results and believe that its control accuracy and loading performance are better than those of the original old load simulator.
    publisherASCE
    titleIntelligent Dynamic Force Loading Algorithm for Aerospace Rudder Load Simulator
    typeJournal Article
    journal volume36
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4466
    journal fristpage04023060-1
    journal lastpage04023060-20
    page20
    treeJournal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005
    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