公开(公告)号：US20240265815A1

公开(公告)日：2024-08-08

申请号：US18192350

申请日：2023-03-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Suresh Bazawada ,  Anil Kumar Songa ,  Bojanapu Naresh

IPC: G08G5/00

CPC classification number: G08G5/0039 ,  G08G5/0021 ,  G08G5/0086

Abstract: Systems and methods are provided for generating a modified flight to avoid a no turn situation. A current flight path of an aircraft is received from a source of current flight path of the aircraft. Current aircraft location data is received from at least one geospatial sensor of the aircraft. Terrain data is retrieved from an onboard database based on the current aircraft location data. The terrain data includes a first terrain obstacle and a second terrain obstacle. A determination is made regarding whether the current flight path of the aircraft leads to a no turn situation with respect to the first terrain obstacle and the second terrain obstacle. A first notification associated with implementation of a modified flight path in accordance with a viable turn with respect to the first terrain obstacle and the second terrain obstacle is displayed on an onboard display device based on the determination.