RESONANT WINGBEAT TUNING CIRCUIT USING STRAIN-RATE FEEDBACK FOR ORNITHOPTIC MICRO AERIAL VEHICLES
    1.
    发明申请
    RESONANT WINGBEAT TUNING CIRCUIT USING STRAIN-RATE FEEDBACK FOR ORNITHOPTIC MICRO AERIAL VEHICLES 失效
    使用应变速率反馈的微波智能调谐电路

    公开(公告)号:US20050001091A1

    公开(公告)日:2005-01-06

    申请号:US10693848

    申请日:2003-10-14

    Applicant: David Raney

    Inventor: David Raney

    CPC classification number: B64C39/028 B64C33/02 B64C2201/025

    Abstract: A resonant wingbeat tuning circuit automatically tunes the frequency of an actuating input to the resonant frequency of a flexible wing structure. Through the use of feedback control, the circuit produces the maximum flapping amplitude of a mechanical ornithoptic system, tracking the resonant frequency of the vibratory flapping apparatus as it varies in response to changes in flight condition, ambient pressure, or incurred wing damage.

    Abstract translation: 谐振式颤振调谐电路将启动输入的频率自动调谐到柔性翼结构的谐振频率。 通过使用反馈控制,电路产生机械鸟瞰图系统的最大拍动幅度,跟踪振动扑动装置的谐振频率,因为其响应于飞行状态,环境压力或所造成的翼损坏的变化而变化。

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