公开(公告)号：US07840316B2

公开(公告)日：2010-11-23

申请号：US11957665

申请日：2007-12-17

申请人： Larry J. Yount ,  Gerald B. Kelley ,  Kent A. Stange ,  Welsh C. Pond

发明人： Larry J. Yount ,  Gerald B. Kelley ,  Kent A. Stange ,  Welsh C. Pond

IPC分类号： G01C23/00

CPC分类号： B64C13/503 ,  G05D1/0061

摘要： An aircraft flight control surface actuation control system includes an actuator control unit and a flight control module. The actuator control unit includes at least two independent actuator control channels to generate limited authority flight control surface actuator commands based on pilot inceptor position signals and flight control augmentation data. The flight control module supplies the flight control augmentation data to each of the independent actuator control channels, determines operability of each of the actuator control channels and, based on the determined operability of each independent actuator control channel, selectively prevents one of the independent actuator control channels from supplying the limited authority flight control surface actuator commands. The flight control module may also generate full authority flight control surface actuator commands for supply to flight control surface actuators.

摘要翻译： 飞行器飞行控制表面致动控制系统包括致动器控制单元和飞行控制模块。 致动器控制单元包括至少两个独立的致动器控制通道，用于基于导向受体位置信号和飞行控制增强数据产生有限的授权的飞行控制表面致动器命令。 飞行控制模块将飞行控制增强数据提供给每个独立的致动器控制通道，确定每个致动器控制通道的可操作性，并且基于所确定的每个独立致动器控制通道的可操作性，选择性地防止独立致动器控制 提供有限授权飞行控制表面执行器命令的通道。 飞行控制模块还可以产生用于向飞行控制表面致动器供应的完全授权的飞行控制表面致动器命令。

公开(公告)号：US20090152404A1

公开(公告)日：2009-06-18

申请号：US11957665

申请日：2007-12-17

申请人： Larry J. Yount ,  Gerald B. Kelley ,  Kent A. Stange ,  Welsh C. Pond

发明人： Larry J. Yount ,  Gerald B. Kelley ,  Kent A. Stange ,  Welsh C. Pond

IPC分类号： G05D1/00

CPC分类号： B64C13/503 ,  G05D1/0061

摘要： An aircraft flight control surface actuation control system includes an actuator control unit and a flight control module. The actuator control unit includes at least two independent actuator control channels to generate limited authority flight control surface actuator commands based on pilot inceptor position signals and flight control augmentation data. The flight control module supplies the flight control augmentation data to each of the independent actuator control channels, determines operability of each of the actuator control channels and, based on the determined operability of each independent actuator control channel, selectively prevents one of the independent actuator control channels from supplying the limited authority flight control surface actuator commands. The flight control module may also generate full authority flight control surface actuator commands for supply to flight control surface actuators.

摘要翻译： 飞行器飞行控制表面致动控制系统包括致动器控制单元和飞行控制模块。 致动器控制单元包括至少两个独立的致动器控制通道，用于基于导向受体位置信号和飞行控制增强数据产生有限的授权的飞行控制表面致动器命令。 飞行控制模块将飞行控制增强数据提供给每个独立的致动器控制通道，确定每个致动器控制通道的可操作性，并且基于所确定的每个独立致动器控制通道的可操作性，选择性地防止独立致动器控制 提供有限授权飞行控制表面执行器命令的通道。 飞行控制模块还可以产生用于向飞行控制表面致动器供应的完全授权的飞行控制表面致动器命令。