The invention discloses a yaw control method and mechanism for a bionic miniature flapping-wing aircraft. According to the yaw control method and the mechanism, a yaw control principle of insect and bee bird flight in the nature is imitated, the actual vibration properties of the miniature flapping-wing aircraft are considered, a corresponding control mechanism is designed based on the yaw controlmethod of the bionic micro flapping-wing aircraft, two mechanism design schemes of single-steering-engine and double-steering-engine yaw control are provided, the wings are directly operated by meansof the steering engines, and yaw control over the bionic miniature flapping-wing aircraft is achieved. Compared with an existing bionic miniature flapping-wing aircraft yawing control method and mechanism, yawing control over wings is directly operated, the control mechanism is easy to implement and operate, and the requirements for small size and light weight of the bionic miniature flapping-wing aircraft are better met.

    本发明公开了一种仿生微型扑翼飞行器偏航控制方法和机构。本发明仿造自然界中的昆虫及蜂鸟飞行的偏航控制原理,考虑了微型扑翼飞行器实际振动特性,并基于该仿生微型扑翼飞行器偏航控制方法设计了相应的控制机构,并提出了单舵机和双舵机偏航控制两种机构设计方案,通过舵机直接对翼进行操作,实现仿生微型扑翼飞行器的偏航控制。相比现有的仿生微型扑翼飞行器偏航控制方法和机构,本发明偏航控制对翼直接操作、控制机构实现简单,操作容易,更加符合仿生微型扑翼飞行器体积小、重量轻的要求。


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    Title :

    Yaw control method and mechanism for bionic miniature flapping-wing aircraft


    Additional title:

    一种仿生微型扑翼飞行器偏航控制方法和机构


    Contributors:
    WU JIANGHAO (author) / CAO HEYU (author)

    Publication date :

    2020-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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