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11.
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
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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公开(公告)号:US10797945B2
公开(公告)日:2020-10-06
申请号:US15884835
申请日:2018-01-31
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Phillip Toews , Rajeev Mohan , Ravish Udupa , Richard Snyder , Robert Brownlee , Brian Walter , Daniel E. Lewis
Abstract: Methods for providing a flight management service in a cloud computing environment, the method includes: receiving, an object request by a server from a mobile device wherein the server is located in the cloud computing environment including: at least a flight management system (FMS) connected to a stateless object; processing, by the connected FMS hosted by the server, the object request generating a resource object for a particular flight plan wherein the resource object includes a data set; storing, by the connected FMS, the data set at the stateless object in the cloud environment; and sending, by the server, an object response from the connected FMS to the mobile device, for accessing the data set of the stateless object for the particular flight plan.
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13.
公开(公告)号:US20190213891A1
公开(公告)日:2019-07-11
申请号:US15867666
申请日:2018-01-10
Applicant: Honeywell International Inc.
Inventor: Richard Snyder , Rajeev Mohan , Rajesh Chaubey , Ravish Udupa , Sharanabasappa Advani
IPC: G08G5/00
CPC classification number: G08G5/0039 , G08G5/0013 , G08G5/0021 , G08G5/0026 , G08G5/006 , G08G5/0078 , G08G5/0082 , G08G5/0091 , G08G5/025
Abstract: A system and methods for enhancing operator situational awareness are disclosed. For example, one method includes monitoring a plurality of radio transmissions associated with a plurality of vehicles in a first traffic flow pattern, monitoring a second traffic flow pattern in a vicinity of a vehicle of the plurality of vehicles, monitoring at least one weather value for a destination site for the plurality of vehicles, proposing a destination approach for the vehicle in response to the monitoring, evaluating an impact of the proposed destination approach on an existing travel path for the vehicle, and generating a second travel path for the vehicle in response to the evaluating.
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14.
公开(公告)号:US20190152619A1
公开(公告)日:2019-05-23
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
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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15.
公开(公告)号:US20190049268A1
公开(公告)日:2019-02-14
申请号:US15675256
申请日:2017-08-11
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Rajeev Mohan , Ravish Udupa , Ruben Carrillo , Shashi Kumar Namde
Abstract: A method and system for aircraft management for selecting a speeding profile mode for phases of a flight plan including: retrieving assigned space goals (ASG) corresponding to a plurality of achieve by point (ABP) designations for a target flight path of the aircraft wherein the target flight path is associated with a target aircraft; determining a target air speed and applicable speed profile modes by retrieving prior information of traffic history and flight plans of the target aircraft to achieve the ABP designations corresponding to an ASG retrieved; selecting from a plurality of applicable speed profile modes, at least one applicable speed profile mode for a phase of the target flight plan for the aircraft; and comparing statuses of the aircraft of at least a status of fuel remaining for a combination of the selection of the applicable speed profile mode and the phase of the target flight plan.
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