公开(公告)号：US09546002B1

公开(公告)日：2017-01-17

申请号：US14041368

申请日：2013-09-30

Applicant: The Boeing Company

Inventor： Brian Azcuenaga ,  Samantha A. Schwartz ,  Jason W. Clark ,  Matthew B. Hendrian ,  Willard K. Otto

IPC: G06K9/62 ,  B64D43/00 ,  B64D47/08

CPC classification number: B64D43/00 ,  B64D47/08 ,  G01C23/00 ,  G06K9/00832 ,  G06K2209/03

Abstract: An instrument panel is identified based on a captured image such as a photograph. A target configuration of the instrument panel is compared with a current configuration of the instrument panel based on the image data. An indication of differences between the target configuration and the current configuration is provided.

Abstract translation: 基于诸如照片的捕获图像来识别仪表板。 基于图像数据将仪表板的目标配置与仪表板的当前配置进行比较。 提供目标配置和当前配置之间的差异的指示。

公开(公告)号：US20230386346A1

公开(公告)日：2023-11-30

申请号：US17825195

申请日：2022-05-26

Applicant: THE BOEING COMPANY

Inventor： Samantha Schwartz ,  Millie Irene Sterling ,  Theresa Emsbach ,  Brian Azcuenaga ,  Jeffrey Lee Williams ,  Aaron Pilcher

IPC: G08G5/00 ,  G01C21/20

CPC classification number: G08G5/0039 ,  G08G5/0021 ,  G01C21/20 ,  G06F3/0482

Abstract: A system and a method include a rerouting control unit configured to generate one or more reroute options for an aircraft based on an analysis of a current position of the aircraft, a predicted future position of the aircraft, a current position of an in-flight hazard, a predicted future position of the in-flight hazard, and one or both of: (i) a flight path of one or more other aircraft within an airspace, or (ii) one or both of a minimum amount of fuel of the aircraft or a minimum weight of the aircraft at a destination location.

公开(公告)号：US10909858B2

公开(公告)日：2021-02-02

申请号：US16145705

申请日：2018-09-28

Applicant: THE BOEING COMPANY

Inventor： Samantha Schwartz ,  Melissa Irene Blackstun ,  Theresa Ernsbach ,  Brian Azcuenaga ,  Stephen Solomon Altus ,  Aaron Pilcher ,  Jeffrey Lee Williams

IPC: G08G5/00 ,  B64D45/00

Abstract: An aircraft management system and method includes a flight plan diversion prediction system including a rerouting control unit that is configured to generate one or more reroute options for an aircraft based on an analysis of a current position of the aircraft, a predicted future position of the aircraft, a current position of an in-flight hazard, and a predicted future position of the in-flight hazard.