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1. 发明授权

US07840316B2 Limited authority and full authority mode fly-by-wire flight control surface actuation control system 有权
标题翻译：有限权限和全权限模式飞控飞行控制面启动控制系统
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。

2. 发明申请

US20090152404A1 LIMITED AUTHORITY AND FULL AUTHORITY MODE FLY-BY-WIRE FLIGHT CONTROL SURFACE ACTUATION CONTROL SYSTEM 有权
标题翻译：有限责任权和全权证模式飞行式飞行控制表面执行控制系统
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。

3. 发明申请

US20080022151A1 METHODS AND SYSTEMS FOR PROVIDING RECONFIGURABLE AND RECOVERABLE COMPUTING RESOURCES 有权
标题翻译：提供可重构和可恢复计算资源的方法和系统
公开(公告)号：US20080022151A1
公开(公告)日：2008-01-24
申请号：US11458301
申请日：2006-07-18
申请人： Kent Stange , Richard Hess , Gerald B. Kelley , Randy Rogers
发明人： Kent Stange , Richard Hess , Gerald B. Kelley , Randy Rogers
IPC分类号： G06F11/00
CPC分类号： G06F11/1494 , G06F11/18
摘要： A method for optimizing the use of digital computing resources to achieve reliability and availability of the computing resources is disclosed. The method comprises providing one or more processors with a recovery mechanism, the one or more processors executing one or more applications. A determination is made whether the one or more processors needs to be reconfigured. A rapid recovery is employed to reconfigure the one or more processors when needed. A computing system that provides reconfigurable and recoverable computing resources is also disclosed. The system comprises one or more processors with a recovery mechanism, with the one or more processors configured to execute a first application, and an additional processor configured to execute a second application different than the first application. The additional processor is reconfigurable with rapid recovery such that the additional processor can execute the first application when one of the one more processors fails.
摘要翻译：公开了一种用于优化数字计算资源的使用以实现计算资源的可靠性和可用性的方法。该方法包括向一个或多个处理器提供恢复机制，所述一个或多个处理器执行一个或多个应用。确定一个或多个处理器是否需要重新配置。当需要时，采用快速恢复来重新配置一个或多个处理器。还公开了一种提供可重新配置和可恢复的计算资源的计算系统。该系统包括具有恢复机制的一个或多个处理器，其中一个或多个处理器被配置为执行第一应用，以及被配置为执行不同于第一应用的第二应用的附加处理器。附加处理器可重新配置，具有快速恢复，使得当多个处理器中的一个失败时，附加处理器可以执行第一应用。

4. 发明授权

US5099412A Automatic control of a discrete system with redundancy management and prioritized conflict resolution 失效
标题翻译：具有冗余管理和优先冲突解决能力的离散系统的自动控制
公开(公告)号：US5099412A
公开(公告)日：1992-03-24
申请号：US414534
申请日：1989-09-29
申请人： Gerald B. Kelley
发明人： Gerald B. Kelley
IPC分类号： G05B13/02 , G05D1/00
CPC分类号： G05D1/0077 , G05B13/0265
摘要： A computer control system in which each input condition to which the system must respond is defined and a priority value assigned thereto. Desired system resource conditions called attributes herein corresponding to each input are determined. System resource states or attributes for all combinations of control element states are determined. An optimum configuration for the discrete control elements is established for a set of input conditions by comparing the system resource condition for each control element configuration with the system resource condition desired for all the input conditions. A score for each input condition is determined based on the priority of the input condition and the number of resource conditions for the input condition which match the resource conditions for a control elements configuration, and the optimum control configuration is the configuration which produces the highest cumulative score for all input conditions.

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