The invention discloses a flapping-wing-based miniature airship and a motion control method thereof. The miniature airship comprises an air bag of a spherical structure, and at least two flapping-wing power systems are arranged at the position, close to the lower portion of the middle line, of the air bag at intervals; the flapping wing power system comprises a fuselage arranged on the air bag and flapping wing assemblies symmetrically arranged on the two sides of the fuselage. The flapping wing assembly comprises a piezoelectric actuator and bionic wings, the first end of the piezoelectric actuator is connected with the fuselage, and the bionic wings are arranged at the second end of the piezoelectric actuator so as to vibrate under the driving of the piezoelectric actuator. The miniature airship is applied to the field of miniature aircrafts and airships, the miniature airship is small in size, light in weight and capable of achieving self-stabilization and long-time endurance, and controllable movement of the miniature airship can be achieved by controlling movement of the flapping wing power system.

    本发明公开了一种基于扑翼式的微型飞艇及其运动控制方法,该微型飞艇包括球状结构的气囊,所述气囊上中线靠下的位置间隔设有至少两个扑翼动力系统;所述扑翼动力系统包括设在所述气囊上的机身,以及对称设在所述机身两侧的扑翼组件;所述扑翼组件包括压电驱动器与仿生翅膀,所述压电驱动器的第一端与所述机身相连,所述仿生翅膀设在所述压电驱动器的第二端,以在所述压电驱动器的驱动下振动。本发明应用于微型飞行器及飞艇领域,该微型飞艇不仅体积小、质量轻,而且可可自稳定同时还可较长时间续航,通过对扑翼动力系统进行运动控制,还可实现微型飞艇的可控运动。


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    Titel :

    Flapping-wing-based miniature airship and motion control method thereof


    Weitere Titelangaben:

    基于扑翼式的微型飞艇及其运动控制方法


    Beteiligte:
    WU YULIE (Autor:in) / XIAO DINGBANG (Autor:in) / WU XUEZHONG (Autor:in) / LU XIANG (Autor:in) / CHEN YANG (Autor:in)

    Erscheinungsdatum :

    2024-01-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64C AEROPLANES , Flugzeuge



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