SYSTEMS AND METHODS FOR AUTHENTICATING DATA TRANSMISSIONS TO VEHICLES

    公开(公告)号:US20240291817A1

    公开(公告)日:2024-08-29

    申请号:US18650259

    申请日:2024-04-30

    IPC分类号: H04L9/40 H04W4/40 H04W12/06

    摘要: Systems and methods for authenticating data transmissions are provided, such as e.g., analog radio streams received at a vehicle. In one aspect, the vehicle includes features that allow for detection and decryption of an encrypted source identifier embedded or introduced into a data transmission transmitted to the vehicle. The source identifier may be used to determine whether the source is authorized to transmit data transmissions to the vehicle and the data transmission may be authenticated accordingly. In another aspect, the vehicle includes features that determine the location of the transmitting device used to transmit the data transmission to the vehicle. The location is then used to determine whether the data transmission should be authenticated.

    Method and system for the updating of a flight plan

    公开(公告)号:US11887487B2

    公开(公告)日:2024-01-30

    申请号:US16925480

    申请日:2020-07-10

    IPC分类号: G08G5/00

    摘要: A method for updating a flight plan comprising, via an avionics device, at least a portion of a flight plan from an external source, authenticating or validating the update, generating a set of updated flight parameters, comparing the set of updated flight parameters with a current set of flight parameters, receiving a set of environmental conditions, performing a series of plausibility checks and automatically updating at least a portion of the flight plan or generating an indication.

    Flight management system and method of updating flight calculations

    公开(公告)号:US11597533B2

    公开(公告)日:2023-03-07

    申请号:US16679537

    申请日:2019-11-11

    IPC分类号: B64D45/00 G06F16/903 G08G5/00

    摘要: A method and apparatus for recording flight information of aircraft, such as position, mass, or type, in order to record the position of a wake turbulence of the aircraft. Weather information can be recorded as affecting the wake turbulence. Such information can be provided into a model or algorithm to determine a path of a wake turbulence. An aircraft on a flight path to encounter the wake turbulence can determine a vortex magnitude of the wake turbulence and determine if an advisory alert needs to be provided if the vortex magnitude satisfies a predetermined threshold.