公开(公告)号：US20190066518A1

公开(公告)日：2019-02-28

申请号：US15683267

申请日：2017-08-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rajesh Chenchu ,  Durga Prasad Dhulipudi ,  Vijaya Bhaskar Ramisetti ,  Reshma Seelam ,  Amit Srivastav ,  Don Nicholas

IPC: G08G5/00 ,  G08G5/04

CPC classification number: G08G5/0034 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0086 ,  G08G5/045

Abstract: A method for validating an operational flight path of an aircraft has been developed. First, a flight path for the aircraft is created using navigation, terrain and obstacle data retrieved from off-line databases. Next, real-time terrain and obstacle update information is captured from flight data sensors on board the aircraft while in flight. Also, light direction and range (LIDAR) data from LIDAR sensors on board the aircraft is collected. A boundary profile is calculated for the flight path based upon the real-time terrain and obstacle update information in combination with the LIDAR data. The flight path is validated using the boundary profile. The results of the validation of the flight path is generated as a report for the aircraft crew.

公开(公告)号：US20170372623A1

公开(公告)日：2017-12-28

申请号：US15194263

申请日：2016-06-27

Applicant: Honeywell International Inc.

Inventor： Amit Srivastav ,  Krishna Idupunur ,  Sibu Parakkattu Narayanan ,  Anantha Chandrasekhar Koduru ,  Shafi Merchant

IPC: G08G5/00 ,  G06Q30/02

CPC classification number: G08G5/0091 ,  G01S13/953 ,  G01W1/02 ,  G01W2001/006 ,  G01W2203/00 ,  G06Q30/0283 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  Y02A90/14 ,  Y02A90/18

Abstract: A system for data aggregation and distribution comprises a context builder that receives a data request from a consumer, and a producers locator that communicates with producers. A producers filter receives a list of producers and selects producers capable of providing data relevant to context information. A data requests formatter receives the context information, and sends the data request to the selected producers. A data responses validator validates data responses from producers, and a data responses processor processes validated data responses. A data predictor receives processed data responses and context information, and generates data prediction information. A data fusion module receives processed data responses, context information, data prediction information, and data history. The data fusion module combines processed data responses with data prediction information to generate a consolidated data response for the consumer. The data fusion module also considers data prediction information upon receiving a request for predicted data when real-time data is unavailable.

公开(公告)号：US20170217605A1

公开(公告)日：2017-08-03

申请号：US15012728

申请日：2016-02-01

Applicant: Honeywell International Inc.

Inventor： Amit Srivastav ,  John Hajdukiewicz ,  Sreedhar Garbham ,  Raman Srinivasan

IPC: B64D45/08 ,  G06T15/00 ,  G01S13/90 ,  G01S19/15 ,  G08G5/00

CPC classification number: B64D45/08 ,  B64D45/04 ,  B64F1/18 ,  G01S7/003 ,  G01S7/20 ,  G01S13/86 ,  G01S13/90 ,  G01S13/913 ,  G01S19/15 ,  G01S2013/9064 ,  G06T15/005 ,  G06T2200/04 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0047 ,  G08G5/025

Abstract: Systems and methods of precision landing in adverse conditions are provided. In one embodiment, a precision landing system comprises a vehicle including: a receiver configured to receive position information for structures and a landing zone of a landing site and a processor coupled to a memory, the memory includes three-dimensional geometric structural information for a landing site. The processor configured to: receive the position information from the receiver; assign geographical coordinates to the three-dimensional geometric structural information using the position information for the structures and the landing zone of the landing site; send the three-dimensional geometric structural information and graphical rendering information to a display device. The vehicle further includes a display device, wherein the display device is configured to render and display a three-dimensional representation of the landing site in real-time based on the three-dimension geometric structural information and the graphical rendering information from the processor.

公开(公告)号：US09424754B2

公开(公告)日：2016-08-23

申请号：US14466548

申请日：2014-08-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Amit Srivastav ,  Roger W. Burgin ,  Dave Pepitone

IPC: G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  G08G5/00 ,  G09B9/08 ,  G08G5/02

CPC classification number: G08G5/0021 ,  G01C23/005 ,  G08G5/025 ,  G09B9/08

Abstract: Methods and systems are provided for providing procedure information associated with an aircraft procedure onboard an aircraft. An exemplary method involves obtaining a briefing sequence for the aircraft procedure and providing the procedure information via the output device, wherein the procedure information is provided in accordance with the briefing sequence. When the output device is realized as an audio output device, the procedure information is sequentially provided auditorily via the audio output device. In one or more embodiments, the procedure information is sequentially indicated on a display device onboard the aircraft in concert with the auditorily provided procedure information.

Abstract translation: 提供了用于提供与飞机上的飞行器程序相关联的程序信息的方法和系统。 一种示例性方法包括获得飞行器程序的简报顺序并经由输出装置提供程序信息，其中根据简报顺序提供程序信息。 当输出装置被实现为音频输出装置时，通过音频输出装置顺序提供程序信息。 在一个或多个实施例中，程序信息在听觉提供的程序信息的一致性下依次表示在飞机上的显示设备上。