MODEL BASED SENSOR SYSTEM FOR LOADS AWARE CONTROL LAWS
    1.
    发明公开
    MODEL BASED SENSOR SYSTEM FOR LOADS AWARE CONTROL LAWS 审中-公开
    MODEMBASIERTES SENSORSYSTEMFÜRLASTENBEWUSSTE STEUERUNGSREGELN

    公开(公告)号:EP2168022A4

    公开(公告)日:2013-06-05

    申请号:EP08827787

    申请日:2008-05-30

    IPC分类号: G05D1/08 B64C27/57 G05D3/10

    CPC分类号: B64C27/57 G05D1/0858

    摘要: A flight control system includes a model-based sensor system which estimates angular accelerations to control rotor system moment such that loads on the aircraft structure are reduced to thereby allow an aircraft structural envelope to more closely follow an aircraft service flight envelope.

    摘要翻译: 飞行控制系统包括基于模型的传感器系统,其估计角加速度以控制转子系统时刻,使得飞行器结构上的载荷减小,从而允许飞行器结构信封更紧密地遵循飞机服务飞行信封。