公开(公告)号：US08935015B2

公开(公告)日：2015-01-13

申请号：US13308818

申请日：2011-12-01

Applicant: Jonathan S. Olsoe ,  David McLaughlin ,  Charles B. Hartin ,  Luc Cyrot ,  Bruce Streeter ,  Stephane Wanchu

Inventor： Jonathan S. Olsoe ,  David McLaughlin ,  Charles B. Hartin ,  Luc Cyrot ,  Bruce Streeter ,  Stephane Wanchu

IPC: G05D1/00 ,  B64C13/42 ,  B64C13/50

CPC classification number: G05D1/0077 ,  B64C13/42 ,  B64C13/503

Abstract: A flight control system and method including a primary flight control path between one or more pilot controls and control surface actuators on an associated aircraft, wherein the primary control path includes one or more flight control computers and one or more first data concentrators; and a secondary flight control path between the one or more pilot controls and the control surface actuators, wherein the secondary flight control path utilizes direct mode control laws to control the control surface actuators; wherein the primary flight control path and the secondary flight control path are independent from each other and the secondary flight control path is operative upon detection of a fault in the primary flight control path.

Abstract translation: 一种飞行控制系统和方法，包括一个或多个先导控制和相关飞行器上的控制表面致动器之间的主飞行控制路径，其中所述主控制路径包括一个或多个飞行控制计算机和一个或多个第一数据集中器; 以及在所述一个或多个引导控制和所述控制表面致动器之间的次要飞行控制路径，其中所述次要飞行控制路径利用直接模式控制定律来控制所述控制表面致动器; 其中所述主飞行控制路径和所述次飞行控制路径彼此独立，并且所述辅助飞行控制路径在检测到所述主飞行控制路径中的故障时操作。

公开(公告)号：US20120290153A1

公开(公告)日：2012-11-15

申请号：US13308818

申请日：2011-12-01

Applicant: Jonathan S. Olsoe ,  David McLaughlin ,  Charles B. Hartin ,  Luc Cyrot ,  Bruce Streeter ,  Stephane Wanchu

Inventor： Jonathan S. Olsoe ,  David McLaughlin ,  Charles B. Hartin ,  Luc Cyrot ,  Bruce Streeter ,  Stephane Wanchu

IPC: G05D1/00

CPC classification number: G05D1/0077 ,  B64C13/42 ,  B64C13/503

Abstract: A flight control system and method including a primary flight control path between one or more pilot controls and control surface actuators on an associated aircraft, wherein the primary control path includes one or more flight control computers and one or more first data concentrators; and a secondary flight control path between the one or more pilot controls and the control surface actuators, wherein the secondary flight control path utilizes direct mode control laws to control the control surface actuators; wherein the primary flight control path and the secondary flight control path are independent from each other and the secondary flight control path is operative upon detection of a fault in the primary flight control path.

Abstract translation: 一种飞行控制系统和方法，包括一个或多个先导控制和相关飞行器上的控制表面致动器之间的主飞行控制路径，其中所述主控制路径包括一个或多个飞行控制计算机和一个或多个第一数据集中器; 以及在所述一个或多个引导控制和所述控制表面致动器之间的次要飞行控制路径，其中所述次要飞行控制路径利用直接模式控制定律来控制所述控制表面致动器; 其中所述主飞行控制路径和所述次飞行控制路径彼此独立，并且所述辅助飞行控制路径在检测到所述主飞行控制路径中的故障时操作。

公开(公告)号：US07337044B2

公开(公告)日：2008-02-26

申请号：US10985028

申请日：2004-11-10

Applicant: Jean-Paul Platzer ,  Stephane Wanchu

Inventor： Jean-Paul Platzer ,  Stephane Wanchu

IPC: G01C23/00

CPC classification number: G05D1/0077

Abstract: A flight control computer for controlling an actuator responsive to a flight control command is described. The system includes a first, second, and third pair of processors. Three different processor types make up the three pairs of processors and the pairs of processors differ between all processor pairs. A method aspect of providing a robust flight control computer controlling actuator responsive to a flight control command includes arranging interconnected pairs of processors using different processor types such that the pairs of processors differ between all processor pairs. An identical flight control command is received at each processor pair. A processor pair is declared to be in failure and processing is transferred to another processor pair if the compared output of each processor pair after receiving the identical flight control command differs between the processors in the pair.

Abstract translation: 描述了用于响应于飞行控制命令来控制致动器的飞行控制计算机。 该系统包括第一，第二和第三对处理器。 三种不同的处理器类型组成三对处理器，并且处理器对之间的处理器对不同。 提供响应于飞行控制命令的强大的飞行控制计算机控制致动器的方法方面包括使用不同的处理器类型布置互连的处理器对，使得所述处理器对之间的处理器对不同。 在每个处理器对处接收相同的飞行控制命令。 如果在接收相同的飞行控制命令之后的每个处理器对的比较输出在对中的处理器之间不同，则处理器对被声明为处于故障状态并且处理被传送到另一个处理器对。

公开(公告)号：US20060100750A1

公开(公告)日：2006-05-11

申请号：US10985028

申请日：2004-11-10

Applicant: Jean-Paul Platzer ,  Stephane Wanchu

Inventor： Jean-Paul Platzer ,  Stephane Wanchu

IPC: G01C23/00

CPC classification number: G05D1/0077

Abstract: A flight control computer for controlling an actuator responsive to a flight control command is described. The system includes a first, second, and third pair of processors. Three different processor types make up the three pairs of processors and the pairs of processors differ between all processor pairs. A method aspect of providing a robust flight control computer controlling actuator responsive to a flight control command includes arranging interconnected pairs of processors using different processor types such that the pairs of processors differ between all processor pairs. An identical flight control command is received at each processor pair. A processor pair is declared to be in failure and processing is transferred to another processor pair if the compared output of each processor pair after receiving the identical flight control command differs between the processors in the pair.

Abstract translation: 描述了用于响应于飞行控制命令来控制致动器的飞行控制计算机。 该系统包括第一，第二和第三对处理器。 三种不同的处理器类型组成三对处理器，并且处理器对之间的处理器对不同。 提供响应于飞行控制命令的强大的飞行控制计算机控制致动器的方法方面包括使用不同的处理器类型布置互连的处理器对，使得所述处理器对之间的处理器对不同。 在每个处理器对处接收相同的飞行控制命令。 如果在接收相同的飞行控制命令之后的每个处理器对的比较输出在对中的处理器之间不同，则处理器对被声明为处于故障状态并且处理被传送到另一个处理器对。