公开(公告)号：US20160004501A1

公开(公告)日：2016-01-07

申请号：US14321562

申请日：2014-07-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Satyanarayan Kar ,  Stephen Mead ,  Anupam Mazumdar

IPC: G06F3/16 ,  G10L25/51 ,  G10L25/27 ,  G10L15/22

CPC classification number: G06F3/167 ,  B64D11/00155 ,  B64D11/0626 ,  B64D2011/0053 ,  G10L15/193 ,  G10L15/22 ,  G10L25/27 ,  G10L25/51 ,  G10L2015/223

Abstract: Methods and apparatus are provided for generating aircraft cabin control commands from verbal speech onboard an aircraft. An audio command supplied to an audio input device is processed. Each word of the processed audio command is compared to words stored in a vocabulary map to determine a word type of each word. Each determined word type is processed to determine if an intent of the audio command is discernable. If the intent is discernable, an aircraft cabin control command is generated based on the discerned intent. If a partial intent is discernable, feedback is generated.

Abstract translation: 提供了用于从飞机上的语言语音生成飞行器舱控制命令的方法和装置。 处理提供给音频输入设备的音频命令。 将经处理的音频命令的每个字与存储在词汇图中的词进行比较，以确定每个单词的单词类型。 处理每个确定的字类型以确定音频命令的意图是否可辨别。 如果意图是可辨别的，则基于识别的意图产生飞机机舱控制命令。 如果可以辨别出部分意图，则会产生反馈。

公开(公告)号：US20210090446A1

公开(公告)日：2021-03-25

申请号：US16579563

申请日：2019-09-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Abdur Rab ,  Donald Walker ,  Anupam Mazumdar ,  Prashanth Thirumalaivenjamur ,  Arivazhagan V

IPC: G08G5/00 ,  G08G5/06 ,  B64D43/02

Abstract: A method in a trail aircraft for monitoring the separation distance between the trail aircraft and a lead aircraft during a flight deck interval management paired approach (FIM-PA) procedure is provided. The method includes: receiving an assigned spacing goal (ASG); receiving traffic information regarding the lead aircraft that indicates the position, heading and ground velocity of the lead aircraft; retrieving a predetermined tolerance limit and traffic information regarding the trail aircraft that indicates the position, heading and ground velocity of the trail aircraft; setting a range limit that is at least as great as the absolute limit indicated by the ASG plus the tolerance limit; monitoring the range and ground speed differential between the lead aircraft and the trail aircraft; and generating a caution alert indicator when a monitored condition detected from monitoring the range and ground speed differential indicates a potential problem.