公开(公告)号：US11313974B2

公开(公告)日：2022-04-26

申请号：US16814457

申请日：2020-03-10

Applicant: Honeywell International Inc.

Inventor： John D. Savoy, Jr. ,  Harold Anthony Zulch, III ,  Gary Ostrom

IPC: G01S19/21

Abstract: A system comprises processing circuitry configured to receive position data from a global navigation satellite system (GNSS) receiver and to receive a first vehicle height above terrain (HAT) from HAT circuitry. A lateral position and an altitude are derived from the position data. The processing circuitry is further configured to determine terrain elevation based upon the lateral position. The processing circuitry is further configured to determine a second vehicle height above terrain (HAT) based upon subtracting the determined terrain elevation from the altitude. The processing circuitry is further configured to detect GNSS spoofing based upon a difference between the first vehicle HAT and the second vehicle HAT; and upon detecting GNSS spoofing, issue an alert.

公开(公告)号：US20220392358A1

公开(公告)日：2022-12-08

申请号：US17443288

申请日：2021-07-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Harisha Bangalore Manjunath ,  Rushoth Kumar M C ,  Venu Puttam ,  Murali Kadeppagari ,  Prashant Hegde ,  Chandana Venigalla ,  Supratik Gon ,  Brad H. Miller ,  Gary Ostrom ,  Ricardo Darif Bortolini ,  Dhivagar Palanisamy ,  David Kolbet ,  John Vo

IPC: G08G5/00 ,  B64D45/00

Abstract: A system and method for implementing an autonomous distress tracking (ADT) triggering function is provided. The method comprises receiving a configuration file containing a plurality of user configurable parameters from a ground-based system, configuring an aircraft condition and monitoring function (ACMF) engine to apply trigger logic specified by the plurality of user configurable parameters to aircraft sensor and/or system data and monitoring for a plurality of distress conditions specified by the plurality of user configurable parameters; executing the configured ACMF engine to detect the occurrence of a distress condition; automatically generating a data message when a distress condition occurrence has been detected wherein the data message can include aircraft position data specified in the user configurable parameters, the aircraft sensor and/or system data on which the detection of the one or more trigger conditions was based, and the identity of the detected distress condition; and automatically sending the data message to a transmission system onboard the aircraft that is configured to transmit a search and rescue signal.

公开(公告)号：US20210286086A1

公开(公告)日：2021-09-16

申请号：US16814457

申请日：2020-03-10

Applicant: Honeywell International Inc.

Inventor： John D. Savoy, JR. ,  Harold Anthony Zulch, III ,  Gary Ostrom

IPC: G01S19/21

Abstract: A system comprises processing circuitry configured to receive position data from a global navigation satellite system (GNSS) receiver and to receive a first vehicle height above terrain (HAT) from HAT circuitry. A lateral position and an altitude are derived from the position data. The processing circuitry is further configured to determine terrain elevation based upon the lateral position. The processing circuitry is further configured to determine a second vehicle height above terrain (HAT) based upon subtracting the determined terrain elevation from the altitude. The processing circuitry is further configured to detect GNSS spoofing based upon a difference between the first vehicle HAT and the second vehicle HAT; and upon detecting GNSS spoofing, issue an alert.