公开(公告)号：WO2010099521A1

公开(公告)日：2010-09-02

申请号：PCT/US2010/025720

申请日：2010-03-01

Applicant: BELL HELICOPTER TEXTRON INC. ,  HEVERLY, David, E., II ,  SINGH, Rupinder ,  PAPPAS, John

Inventor： HEVERLY, David, E., II ,  SINGH, Rupinder ,  PAPPAS, John

IPC: B64C27/00

CPC classification number: B64C27/001 ,  B64C2027/004 ,  F16F15/002 ,  G10K11/17854 ,  G10K11/17879 ,  G10K11/17883 ,  G10K2210/1281 ,  G10K2210/3012 ,  G10K2210/3055 ,  G10K2210/3056

Abstract: The adaptive reference model algorithm uses a gain scheduling feature combined with a customized Least-Squares routine as an adaptive method for adjusting feedback control so as to account for variations in Transfer Function (G), thereby optimizing the effectiveness of the Active Vibration Control (AVC) System. The Least- Squares routine identifies the transfer function in a background process without interruption of closed loop vibration control. This identification approach is accomplished without intentional interrogation of the AVC actuators and without intentional vibration level changes. For this adaptive control logic, the dynamic relationship between AVC actuators and AVC sensors is represented by a mathematical model of Transfer Function (G). The mathematical model of Transfer Function (G) is continuously updated by the Least-Squares routine. A feedback gain (H) is computed from the mathematical model of Transfer Function (G), and the feedback gain (H) is updated each time the mathematical model of Transfer Function (G) is updated.

Abstract translation: 自适应参考模型算法使用增益调度特征结合定制的最小二乘例程作为调整反馈控制的自适应方法，以便考虑传递函数（G）的变化，从而优化主动振动控制（AVC）的有效性 ）系统。 最小二乘法例程在后台程序中识别传递函数，而不会中断闭环振动控制。 该识别方法是在没有有意询问AVC致动器而没有有意的振动水平变化的情况下完成的。 对于这种自适应控制逻辑，AVC执行器和AVC传感器之间的动态关系由传递函数（G）的数学模型表示。 传递函数（G）的数学模型通过最小二乘例程不断更新。 从传递函数（G）的数学模型计算反馈增益（H），并且每当更新传递函数（G）的数学模型时，反馈增益（H）被更新。

公开(公告)号：EP2401198A1

公开(公告)日：2012-01-04

申请号：EP10746964.5

申请日：2010-03-01

Applicant: Bell Helicopter Textron Inc.

Inventor： HEVERLY, David, E., II ,  SINGH, Rupinder ,  PAPPAS, John

IPC: B64C27/00

CPC classification number: B64C27/001 ,  B64C2027/004 ,  F16F15/002 ,  G10K11/17854 ,  G10K11/17879 ,  G10K11/17883 ,  G10K2210/1281 ,  G10K2210/3012 ,  G10K2210/3055 ,  G10K2210/3056

Abstract: The adaptive reference model algorithm uses a gain scheduling feature combined with a customized Least-Squares routine as an adaptive method for adjusting feedback control so as to account for variations in Transfer Function (G), thereby optimizing the effectiveness of the Active Vibration Control (AVC) System. The Least-Squares routine identifies the transfer function in a background process without interruption of closed loop vibration control. This identification approach is accomplished without intentional interrogation of the AVC actuators and without intentional vibration level changes. For this adaptive control logic, the dynamic relationship between AVC actuators and AVC sensors is represented by a mathematical model of Transfer Function (G). The mathematical model of Transfer Function (G) is continuously updated by the Least-Squares routine. A feedback gain (H) is computed from the mathematical model of Transfer Function (G), and the feedback gain (H) is updated each time the mathematical model of Transfer Function (G) is updated.

公开(公告)号：EP2401198B1

公开(公告)日：2015-07-08

申请号：EP10746964.5

申请日：2010-03-01

Applicant: Bell Helicopter Textron Inc.

Inventor： HEVERLY, David, E., II ,  SINGH, Rupinder ,  PAPPAS, John

IPC: B64C27/00 ,  F16F15/02 ,  G10K11/178

CPC classification number: B64C27/001 ,  B64C2027/004 ,  F16F15/002 ,  G10K11/17854 ,  G10K11/17879 ,  G10K11/17883 ,  G10K2210/1281 ,  G10K2210/3012 ,  G10K2210/3055 ,  G10K2210/3056

Abstract: The adaptive reference model algorithm uses a gain scheduling feature combined with a customized Least-Squares routine as an adaptive method for adjusting feedback control so as to account for variations in Transfer Function (G), thereby optimizing the effectiveness of the Active Vibration Control (AVC) System. The Least-Squares routine identifies the transfer function in a background process without interruption of closed loop vibration control. This identification approach is accomplished without intentional interrogation of the AVC actuators and without intentional vibration level changes. For this adaptive control logic, the dynamic relationship between AVC actuators and AVC sensors is represented by a mathematical model of Transfer Function (G). The mathematical model of Transfer Function (G) is continuously updated by the Least-Squares routine. A feedback gain (H) is computed from the mathematical model of Transfer Function (G), and the feedback gain (H) is updated each time the mathematical model of Transfer Function (G) is updated.

公开(公告)号：EP3150489A1

公开(公告)日：2017-04-05

申请号：EP16190182.2

申请日：2016-09-22

Applicant: Bell Helicopter Textron Inc.

Inventor： HEVERLY, David E. ,  SINGH, Rupinder ,  LEE, Taeoh ,  SMITH, Michael

IPC: B64C27/00

CPC classification number: B64C27/001 ,  B64C27/06 ,  B64C2027/002 ,  B64C2027/004 ,  B64C2027/005 ,  F01D21/003 ,  F01D25/28

Abstract: A vibration control system 200 for a rotorcraft 100 includes at least one of an integrated actuator 208 and an intermediate actuator 210 associated with a first source of vibration, a sensor configured to sense vibration from the first source of vibration, a dedicated actuator 212 configured for association with a fuselage 106, and a controller 204 configured to receive information from the sensor and configured to control the dedicated actuator and the at least one of the integrated actuator and the intermediate actuator.

Abstract translation: 用于旋翼飞行器100的振动控制系统200包括一个集成的致动器208中的至少一个，并与振动的第一源极，被配置为从振动的第一源感测振动的传感器，专用致动器212配置用于关联的中间致动器210 与机身106和配置成接收来自所述传感器的信息和配置成控制所述致动器专用的控制器204和集成致动器的所述至少一个和所述致动器中间关联。