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    Systems and methods for context-specific granular access to flight management system using adaptive identity management
    3.
    发明授权
    Systems and methods for context-specific granular access to flight management system using adaptive identity management 有权

    公开(公告)号：US11856111B2

    公开(公告)日：2023-12-26

    申请号：US17246161

    申请日：2021-04-30

    Applicant: Honeywell International Inc.

    Inventor： Rajeev Mohan ,  Kirupakar Janakiraman

    IPC: H04L9/32 ,  G06F5/00 ,  G06F9/54 ,  G07C5/00

    CPC classification number: H04L9/3268 ,  G06F9/546 ,  G07C5/008 ,  H04L9/3213

    Abstract: Disclosed are methods, systems, and computer-readable medium for context-specific granular access to flight management system (FMS) SaaS using adaptive IAM. For instance, the method may include receiving, at one of a plurality of application programing interface (API) endpoints of a flight management system (FMS) software as a service (SaaS), a request from a client; determining whether the request is authorized; in response to determining the request is authorized, analyzing the request to determine a context of the request and determine whether the request includes an intent; transmitting a message to a particular functionality of the FMS SaaS based on the context and the intent; determining whether the client is associated with a subscription type; filtering a data stream from the FMS SaaS in accordance with the subscription type and the context; generating a response based on the filtered data stream; and transmitting the response to the client.

    Systems and methods for providing or requesting avionics simulation data using API adapter
    6.
    发明授权
    Systems and methods for providing or requesting avionics simulation data using API adapter 有权

    公开(公告)号：US10798189B1

    公开(公告)日：2020-10-06

    申请号：US16385253

    申请日：2019-04-16

    Applicant: Honeywell International Inc.

    Inventor： Mahesh Sivaratri ,  Raghu Shamasundar ,  Rajeev Mohan ,  Sushma Bidrupane ,  Soumitri Swain ,  Mythili Belle

    IPC: G09B9/02 ,  H04L29/08 ,  G09B9/08 ,  H04L29/06

    Abstract: Systems and methods are disclosed for providing or requesting data for simulating avionics systems. For example, a method for providing data for simulating avionics systems may include: receiving, from a client device, a first message requesting information usable by the client device to simulate a functionality of an avionics system, the first message being in a web services data format; converting the first message to an avionics protocol data format to obtain a first converted message; providing the first converted message to a server application; receiving, from the server application, a second message including the requested information, the second message being in the avionics protocol data format; converting the second message to the web services data format to obtain a second converted message; and providing, to the client device, the second converted message.

    SYSTEM FOR DISTRIBUTED FLIGHT MANAGEMENT CAPABILITY
    7.
    发明申请
    SYSTEM FOR DISTRIBUTED FLIGHT MANAGEMENT CAPABILITY 审中-公开

    公开(公告)号：US20190164433A1

    公开(公告)日：2019-05-30

    申请号：US15978832

    申请日：2018-05-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Connor MacDowell ,  Todd Hammer ,  Rajeev Mohan ,  Partho Sarkar ,  Ravish Udupa ,  Richard Snyder

    IPC: G08G5/00

    Abstract: Systems are provided for providing distributed flight management capability for flight management systems (FMS) of a fleet of aircraft. The system comprises an FMS located on board and electronically integrated into the avionics system of each of the aircraft in the fleet. The system also has a digital twin FMS that contains identical software components and capabilities of the FMS. The digital twin FMS is located off board the aircraft and is in communication with each of the FMSs via a digital communications link. The digital twin FMS is configured to provide pre-flight planning for each aircraft that is dispatched to each FMS via the digital communications link.

    SYSTEMS AND METHODS FOR AVERTING OVERWEIGHT AIRCRAFT LANDING CIRCUMSTANCES
    8.
    发明申请
    SYSTEMS AND METHODS FOR AVERTING OVERWEIGHT AIRCRAFT LANDING CIRCUMSTANCES 审中-公开
    用于平稳航空飞行场地电路的系统和方法

    公开(公告)号：US20160031565A1

    公开(公告)日：2016-02-04

    申请号：US14446947

    申请日：2014-07-30

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajeev Mohan ,  Joel Hagen ,  Bhalakrishnan Janardhanan

    IPC: B64D37/12 ,  G07C5/08 ,  G08G5/00

    CPC classification number: B64D37/12 ,  B64D37/26 ,  G07C5/0808 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0047 ,  G08G5/0052

    Abstract: The present disclosure includes a method, article of manufacture, and system for averting an overweight landing of an aircraft having a maximum landing weight (MLW). The method, article, and system may comprise, mutatis mutandis, determining a flight plan, receiving sensor data, determining, in response to the sensor data, that a predetermined event has occurred, receiving, in response to the predetermined event, an updated destination, computing, aircraft weight at the updated destination (WAD), comparing the WAD to the MLW, and/or generating, in response to the sensor data, an updated flight plan when the WAD exceeds the MLW.

    Abstract translation: 本公开包括用于避免具有最大着陆重量（MLW）的飞机的超重着陆的方法，制造品和系统。 方法，物品和系统可以包括：经过必要的修改，确定飞行计划，接收传感器数据，响应于传感器数据确定已发生预定事件，响应于预定事件接收更新的目的地 ，在更新的目的地（WAD）上计算飞机重量，将WAD与MLW进行比较和/或当WAD超过MLW时，响应于传感器数据生成更新的飞行计划。

    System and methods enabling aircraft energy dissipation for rapid decision making
    9.
    发明授权
    System and methods enabling aircraft energy dissipation for rapid decision making 有权

    公开(公告)号：US11790795B2

    公开(公告)日：2023-10-17

    申请号：US16890614

    申请日：2020-06-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Rajeev Mohan ,  Daniel E. Lewis

    IPC: B64D43/02 ,  G08G5/02 ,  G06F3/0482

    CPC classification number: G08G5/025 ,  B64D43/02 ,  G06F3/0482

    Abstract: A method in an aircraft for energy reduction is disclosed. The method includes: determining a starting point location, altitude and airspeed for a stable approach for landing at a diversion airport; and determining a vertical strategy for achieving the starting point altitude and airspeed by identifying a region of opportunity for adjusting the speed and altitude and identifying a plurality of energy reduction strategies for achieving the starting point altitude and airspeed while in the region of opportunity based on a speed mode during the stable approach. The method further comprises causing a graphic display to be displayed that lists for selection each of the plurality of identified strategies, detailed maneuver information for strategy implementation, and costs for implementing each identified strategy; and causing to be displayed, responsive to flight crew selection, a lateral view and vertical view of a proposed trajectory based on a selected identified strategy.

    Method and system for integrating offboard generated parameters into a flight management system
    10.
    发明授权
    Method and system for integrating offboard generated parameters into a flight management system 有权

    公开(公告)号：US10946977B2

    公开(公告)日：2021-03-16

    申请号：US15959485

    申请日：2018-04-23

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajeev Mohan ,  Sreenivasan Govindillam K ,  Srihari Jayathirtha ,  Kalimulla Khan ,  Ravish Udupa

    IPC: G08G5/00 ,  G01C21/00 ,  B64D43/00 ,  B64D45/00

    Abstract: Methods and systems are provided for integrating aircraft flight parameters generated by an offboard portable electronic device (PED) into an onboard flight management system (FMS). The method comprises selecting the aircraft flight parameters to be generated by the PED for use by the FMS. The current flight data is accessed for the aircraft with the FMS and providing the current flight data to the offboard PED. The rules for the aircraft flight parameters are computed with the offboard PED based on the current flight data for the aircraft and transmitted to a flight management (FM) adapter. The FM adapter confirms that the rules for the aircraft flight parameters comply with operational limits of the aircraft and then translates the rules of the aircraft flight parameters to aircraft operational targets for use by the onboard FMS. The aircraft operational targets are then loaded from the FM adapter into the FMS.

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