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    • 2. 发明申请
    • On-demand auto-tuner for a plant control system
    • 用于工厂控制系统的按需自动调谐器
    • US20070073422A1
    • 2007-03-29
    • US11238304
    • 2005-09-29
    • Sujit GaikwadSachi DashKonstantinos Tsakalis
    • Sujit GaikwadSachi DashKonstantinos Tsakalis
    • G05B13/02
    • G05B11/42G05B13/024
    • A method to automatically tune control systems, the method comprising selecting a target loop transfer function for at least one plant subsystem in response to an input excitation, selecting at least one fit-error criterion for a plant subsystem transfer function, and automatically inputting the input excitation and tuning the plant subsystem transfer function to the target loop transfer function. The tuning includes automatically selecting a bandwidth of the plant subsystem transfer function from a plurality of bandwidths determined in accordance with limits of the plant subsystem, inputting the input excitation to the plant subsystem, determining the fit-error of the plant subsystem transfer function to the target loop transfer function in response to the input excitation, and continuing the selecting of a bandwidth in accordance with the fit-error criterion.
    • 一种自动调整控制系统的方法,所述方法包括响应于输入激励为至少一个工厂子系统选择目标循环传递函数,为工厂子系统传递函数选择至少一个拟合误差准则,并自动输入输入 激励和调整工厂子系统传递函数到目标循环传递函数。 调谐包括根据工厂子系统的极限确定的多个带宽自动选择工厂子系统传递函数的带宽,将输入激励输入到工厂子系统,确定工厂子系统传递函数的拟合误差到 响应于输入激励的目标循环传递函数,以及根据拟合误差准则继续选择带宽。
    • 3. 发明申请
    • Model-based detection, diagnosis of turbine engine faults
    • 基于模型的检测,涡轮发动机故障诊断
    • US20050222747A1
    • 2005-10-06
    • US10815036
    • 2004-03-30
    • Mohamad VhoraSachi DashSujit GaikwadDale Mukavetz
    • Mohamad VhoraSachi DashSujit GaikwadDale Mukavetz
    • G05B23/02G06F19/00
    • G05B23/0254G05B23/0281
    • A method of monitoring turbine engines used in aircraft from sensor signals from an engine for a predetermined set of engine characteristics. The signals are transmitted to a nonlinear engine model that predicts the output values for the given set of engine characteristics. The model generates residuals by calculating the difference between the actual values and the predicted values for each member of the set. The generated residuals are evaluated to estimate bounds of uncertainties as indicative of sensor noise. Incoming residuals from ongoing actual engine values are continuously tested against the bounds. A fault is signaled for each of the set of characteristics when a detected bound is exceeded. A computer is used to calculate the fault residual for each of the set of characteristics and the closest fault residual is selected as a diagnosed fault.
    • 一种监测来自发动机的传感器信号的用于飞机的涡轮发动机的方法,用于预定的一组发动机特性。 信号被传送到非线性发动机模型,该非线性发动机模型预测给定的发动机特性集合的输出值。 该模型通过计算实际值和集合中每个成员的预测值之间的差异来生成残差。 评估产生的残差以估计传感器噪声的不确定性界限。 来自持续实际发动机值的进场残差根据界限持续测试。 当超出检测到的边界时,针对该组特征中的每一个发出故障。 计算机用于计算每组特征的故障残差,并选择最接近的故障残差作为诊断故障。