公开(公告)号：US10482772B2

公开(公告)日：2019-11-19

申请号：US15786725

申请日：2017-10-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sanju Kumari ,  Minni Ambooken ,  Subhadeep Pal ,  Nithin Ambika

IPC: G08G5/00 ,  G01C23/00 ,  B64D43/00

Abstract: Methods and systems are provided for generating a flight profile for search and rescue (SAR) operations. The method comprises monitoring flight parameters of an in-flight aircraft engaged in star operations through the aircraft's flight management system (FMS). The flight parameters are transmitted to a ground-based FMS that accesses a terrain database and a real-time weather database. With this information, the ground-based FMS generates a star flight profile for the aircraft. The flight profile is then transmitted to the in-flight aircraft's FMS.

公开(公告)号：US20190318638A1

公开(公告)日：2019-10-17

申请号：US16424089

申请日：2019-05-28

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jayant Kumar Singh ,  Nithin Ambika ,  Subhadeep Pal ,  Saurabh Gohil

IPC: G08G5/04 ,  G08G5/00 ,  G05D1/00 ,  G08G9/02 ,  B64C39/02 ,  G05D1/02

Abstract: A system for providing obstacle alerts to an in-flight aircraft has been developed. The system includes a transceiver on board the vehicle that transmits performance parameters of the vehicle and a remotely located antenna that receives the performance parameters from the transceiver. Also included is a remotely located terrain database stores obstacle characteristics of terrestrial obstacles located in proximity to the vehicle. A remotely located computer system receives the performance parameters from the antenna and the obstacle characteristics in proximity to the vehicle from the terrain database. The computer system calculates a vehicle safety envelope based on the performance parameters and an obstacle safety envelope based on the obstacle characteristics. The computer system generates an obstacle alert for the vehicle if the vehicle safety envelope conflicts with the obstacle safety envelope.

公开(公告)号：US10347141B2

公开(公告)日：2019-07-09

申请号：US15498032

申请日：2017-04-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jayant Kumar Singh ,  Nithin Ambika ,  Subhadeep Pal ,  Saurabh Gohil

IPC: G08G5/04 ,  G08G5/00 ,  G05D1/00 ,  G05D1/02 ,  B64C39/02 ,  G08G9/02 ,  G08G1/16

Abstract: A method for providing obstacle alerts to an in-flight aircraft has been developed. First, parameters of an in-flight aircraft are transmitted to a ground based processor station. The station calculates an aircraft safety envelope based on these parameters. The station accesses the characteristics of obstacles stored in a terrain database and calculates an obstacle safety envelope. Finally, the station determines if the aircraft safety envelope conflicts with the obstacle safety envelope and generates an alert for the aircraft if a conflict exists.

公开(公告)号：US20190114926A1

公开(公告)日：2019-04-18

申请号：US15786725

申请日：2017-10-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sanju Kumari ,  Minni Ambooken ,  Subhadeep Pal ,  Nithin Ambika

IPC: G08G5/00 ,  G01C23/00

CPC classification number: G08G5/0013 ,  B64D43/00 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0039 ,  G08G5/0043 ,  G08G5/0086 ,  G08G5/0091

Abstract: Methods and systems are provided for generating a flight profile for search and rescue (SAR) operations. The method comprises monitoring flight parameters of an in-flight aircraft engaged in star operations through the aircraft's flight management system (FMS). The flight parameters are transmitted to a ground-based FMS that accesses a terrain database and a real-time weather database. With this information, the ground-based FMS generates a star flight profile for the aircraft. The flight profile is then transmitted to the in-flight aircraft's FMS.

公开(公告)号：US20180315324A1

公开(公告)日：2018-11-01

申请号：US15498032

申请日：2017-04-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jayant Kumar Singh ,  Nithin Ambika ,  Subhadeep Pal ,  Saurabh Gohil

IPC: G08G5/04 ,  G08G5/00 ,  G05D1/00 ,  G05D1/02 ,  B64C39/02 ,  G08G9/02

CPC classification number: G08G5/04 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/146 ,  G05D1/0011 ,  G05D1/0088 ,  G05D1/0202 ,  G08G1/165 ,  G08G5/0013 ,  G08G5/0086 ,  G08G9/02

Abstract: A method for providing obstacle alerts to an in-flight aircraft has been developed. First, parameters of an in-flight aircraft are transmitted to a ground based processor station. The station calculates an aircraft safety envelope based on these parameters. The station accesses the characteristics of obstacles stored in a terrain database and calculates an obstacle safety envelope. Finally, the station determines if the aircraft safety envelope conflicts with the obstacle safety envelope and generates an alert for the aircraft if a conflict exists.