利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

2 条记录 (耗时 0.021 秒)

    ROTARY WING AIRCRAFT VIBRATION CONTROL SYSTEM WITH RESONANT INERTIAL ACTUATORS
    1.
    发明申请
    ROTARY WING AIRCRAFT VIBRATION CONTROL SYSTEM WITH RESONANT INERTIAL ACTUATORS 审中-公开
    具有谐振惯性执行器的旋转式飞机振动控制系统

    公开(公告)号：US20130311012A1

    公开(公告)日：2013-11-21

    申请号：US13983463

    申请日：2012-02-03

    申请人： Paul Black ,  Doug Swanson ,  Askari Badre-Alam ,  David Edeal ,  Douglas Pedersen

    发明人： Paul Black ,  Doug Swanson ,  Askari Badre-Alam ,  David Edeal ,  Douglas Pedersen

    IPC分类号： B64C27/00 ,  H02K33/00 ,  H02P25/02

    CPC分类号： B64C27/001 ,  B64C2027/004 ,  F16F7/1011 ,  H02K33/00 ,  H02P25/032

    摘要： A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.

    摘要翻译： 谐振惯性致动器的控制系统基于电压和电流反馈来估计谐振惯性致动器的运行参数，并且动态地限制所选择的参数以维持谐振惯性致动器的安全，有效和成本有效的操作。 根据电压和电流反馈来估计谐振惯性致动器的电驱动器内的电阻，并结合谐振惯性致动器的建模，计算或估计其他操作参数。 考虑到谐振惯性致动器对指令信号变化的响应性，调整指令信号以动态地限制估计的参数。