公开(公告)号：US20130274963A1

公开(公告)日：2013-10-17

申请号：US13926072

申请日：2013-06-25

Applicant: BELL HELICOPTER TEXTRON INC.

Inventor： Shyhpyng Jack Shue ,  John J. Schillings

IPC: B64C19/00

CPC classification number: B64C19/00 ,  G05D1/0858

Abstract: A system includes a plurality of actuators and a control system operably associated with the plurality of actuators. The control system having a control logic architecture having a dynamic command input shaping model associated with an input command, a robust inner loop associated with the dynamic command input shaping model, and a time delay cancellation model. The method includes selecting a control law based upon a flight performance of an aircraft, decoupling the control law into a first individual component and a second individual component of the aircraft flight motion, analyzing each individual component separately, regrouping the component of flight motion, analyzing the control law with a time delay cancellation model and providing the necessary dynamic flight quickness with a different command input condition.

Abstract translation: 系统包括多个致动器和可操作地与多个致动器相关联的控制系统。 所述控制系统具有控制逻辑架构，其具有与输入命令相关联的动态命令输入整形模型，与所述动态命令输入整形模型相关联的鲁棒内部循环，以及时间延迟消除模型。 该方法包括基于飞行器的飞行性能来选择控制律，将控制律解耦到飞行器飞行运动的第一个单独部件和第二个单独部件，分别分析各个部件，重新组合飞行运动的分量，分析 具有时间延迟消除模型的控制规律，并使用不同的命令输入条件提供必要的动态飞行速度。

公开(公告)号：US08942866B2

公开(公告)日：2015-01-27

申请号：US13926072

申请日：2013-06-25

Applicant: Bell Helicopter Textron Inc.

Inventor： Shyhpyng Jack Shue ,  John J. Schillings

IPC: G06F19/00 ,  G01C22/00

CPC classification number: B64C19/00 ,  G05D1/0858

Abstract: A system includes a plurality of actuators and a control system operably associated with the plurality of actuators. The control system having a control logic architecture having a dynamic command input shaping model associated with an input command, a robust inner loop associated with the dynamic command input shaping model, and a time delay cancellation model. The method includes selecting a control law based upon a flight performance of an aircraft, decoupling the control law into a first individual component and a second individual component of the aircraft flight motion, analyzing each individual component separately, regrouping the component of flight motion, analyzing the control law with a time delay cancellation model and providing the necessary dynamic flight quickness with a different command input condition.

Abstract translation: 系统包括多个致动器和可操作地与多个致动器相关联的控制系统。 所述控制系统具有控制逻辑架构，其具有与输入命令相关联的动态命令输入整形模型，与所述动态命令输入整形模型相关联的鲁棒内部循环，以及时间延迟消除模型。 该方法包括基于飞行器的飞行性能来选择控制律，将控制律解耦到飞行器飞行运动的第一个单独部件和第二个单独部件，分别分析各个部件，重新组合飞行运动的分量，分析 具有时间延迟消除模型的控制规律，并使用不同的命令输入条件提供必要的动态飞行速度。