The invention relates to the technical field of aircraft manufacturing, in particular to an inertial navigation three-axis adjusting device which comprises a rotary table base. The first rotating table is rotationally arranged on the rotating table base; the first driving assembly is arranged on the rotary table base; the second rotating table is rotationally arranged on the first rotating table; the second driving assembly is arranged on the first rotating table; the load frame body is rotationally arranged on the second rotating table; the third driving assembly is arranged on the second rotating table; and the balancing assembly is arranged on the second rotating table. According to the method, the accuracy of results of precision calibration and non-zero attitude skewness navigation error analysis can be improved, and meanwhile, the adaptability to different industrial sites is improved.

    本发明涉及飞机制造技术领域,尤其涉及一种惯性导航三轴调节装置,其包括转台底座;第一旋转台,所述第一旋转台转动设置在所述转台底座上;第一驱动组件,所述第一驱动组件设置在所述转台底座上;第二旋转台,所述第二旋转台转动设置在所述第一旋转台上;第二驱动组件,所述第二驱动组件设置在所述第一旋转台上;负载框体,所述负载框体转动设置在所述第二旋转台上;第三驱动组件,所述第三驱动组件设置在所述第二旋转台上;配平组件,所述配平组件设置在所述第二旋转台上。本发明能够提升精度校准和非零位姿态偏度导航误差分析的结果的准确性,同时提升不同工业现场的适应性。


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    Titel :

    Inertial navigation three-axis adjusting device


    Weitere Titelangaben:

    惯性导航三轴调节装置


    Beteiligte:
    LIU YANG (Autor:in) / ZHANG HAO (Autor:in) / ZHU YIMIAO (Autor:in) / ZHANG XIANTAO (Autor:in) / CHEN SHENG (Autor:in) / ZHANG LINLONG (Autor:in)

    Erscheinungsdatum :

    2024-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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