Honeywell International Inc.

Jayasenthilnathan Balasubramanian

Srihari Jayathirtha

Kalimulla Khan

Saravanakumar Gurusamy

Byron F Birkedahl

Madhava Gadicherla

Madhava Gadicheria

Yogiraj Dattaram More

Systems and methods for displaying connectivity strength for vehicles are disclosed. For instance, the method may include receiving, from an off-board station, connectivity data relating to a connected vehicle, the connectivity data having been received from a plurality of connected vehicles other than the connected vehicle and selected based on relevance to the connected vehicle; identifying a portion of the received connectivity data to display on the connected vehicle; generating a display of the identified portion of the received connectivity data; and displaying on a display unit of the connected vehicle, the generated display of the identified portion of the received connectivity data. The method may also include generating and displaying an updated route based on the received connectivity data.

System and method to display connectivity strength and communication performance of connected vehicles

Disclosed are systems, methods, and non-transitory computer-readable medium for providing a safe landing for an aerial vehicle. The method may include: displaying, on one or more displays, an aerial vehicle, an intended landing zone, and a real-time flight path of the vehicle as the vehicle approaches the intended landing zone; receiving data related to one or more of the vehicle, the flight path of the vehicle, the intended landing zone, and an obstacle; determining the proximity of the vehicle relative to the center of the intended landing zone based on the received data; displaying the proximity of the vehicle relative to the center of the intended landing zone; displaying the obstacle when present; displaying an alert when the vehicle deviates in proximity to the center of the intended landing zone and/or approaches the obstacle; and upon determining a failure to respond to the alert computing flight controls to modify landing.

Systems and methods for providing safe landing assistance for an aerial vehicle

Various embodiments described herein relate to performance assurance modeling for a portfolio of assets. In this regard, a request to generate one or more performance assurance insights related to one or more assets is received. The request includes a fault descriptor describing one or more faults associated with the one or more assets. In response to the request, a first risk level associated with the one or more faults is determined based on the fault descriptor and asset data associated with the one or more assets. Additionally, in response to the request, a second risk level associated with the one or more faults is generated based on one or more predetermined relationships between faults and asset performance indicator thresholds. The one or more performance assurance insights are then generated based on a comparison between the first risk level and the second risk level.

Performance metric assurance for asset management

Systems and methods are provided for displaying operating data for a re-chargeable battery for an electric vehicle. The system comprises a re-chargeable battery for powering components of an electrical vehicle, a sensor that detects a present level of charge in the battery and a display. The display receives the present level of charge of the battery from the monitor and displays the present level of charge in the battery, a required level of endurance for the battery that is based on a planned operational parameter for the vehicle, a minimum level of charge in the battery that meets the required level of endurance, and an amount of time needed to re-charge the battery to achieve the minimum level of charge.

System and method for a mission-based battery status display for electric vehicles

Disclosed are methods and systems for identifying and addressing passenger issues in an aircraft. For instance, the method may include receiving sensor data corresponding to one or more sensors associated with a passenger compartment of the aircraft, analyzing the received sensor data to determine a condition of the passenger compartment of the aircraft, identifying one or more passenger issues occurring in the aircraft, and determining one or more response options to address the one or more passenger issues, based at least in part on the one or more passenger issues and an operational parameter of the aircraft. The method may further include communicating, the one or more passenger issues and the one or more response options to a passenger user interface or a ground control station and modifying an operation of the aircraft in accordance with one or more of the one or more response options.

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Phoenix, AZ, United States of America

Jayasenthilnathan Balasubramanian