In this paper, a complete simulation model of steering system of nose landing gear and towbarless traction is established based on LMS Virtual.Lab Motion. And the B737-800 aircraft was taken as the research object to simulate the steering condition of the towbarless traction. The load of the steering system of the nose gear are simulated and analyzed under various steering conditions. The simulation results show the influence of the changes in the steering angle, steering rate and traction rate on the steering system, and provide some reference for further research on the safety of towbarless traction.


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    Title :

    Analysis of effects on the steering system of nose landing gear by towbarless traction


    Contributors:
    Kong, Xiangjie (editor) / Falcone, Francisco (editor) / Huang, Hao (author) / Liu, Hui (author) / Mu, Mengxin (author)

    Conference:

    3rd International Conference on Internet of Things and Smart City (IoTSC 2023) ; 2023 ; Chongqing, China


    Published in:

    Proc. SPIE ; 12708


    Publication date :

    2023-06-14





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English






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