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公开(公告)号：US20210104163A1
公开(公告)日：2021-04-08
申请号：US16945409
申请日：2020-07-31
Applicant: Honeywell International Inc.
Inventor： Richard SNYDER , Rajeev Mohan , Rajesh CHAUBEY , Ravish Udupa , Sharanabasappa Advani
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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公开(公告)号：US10854093B2
公开(公告)日：2020-12-01
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
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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公开(公告)号：US11417222B2
公开(公告)日：2022-08-16
申请号：US16945409
申请日：2020-07-31
Applicant: Honeywell International Inc.
Inventor： Richard Snyder , Rajeev Mohan , Rajesh Chaubey , Ravish Udupa , Sharanabasappa Advani
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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公开(公告)号：US10654589B2
公开(公告)日：2020-05-19
申请号：US15469763
申请日：2017-03-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Rajesh Chaubey , Sharanabasappa Advani , Veeralla Sai V Yashodhar , Ranju Thomas Pulikot , Abhishek Gupta
Abstract: Avionic display systems and methods are provided for generating avionic displays including instability prediction and avoidance symbology, such as dynamically-adjusted drag device deployment cues. In one embodiment, the avionic display system includes a controller and an avionic display device, which is coupled to the controller and on which an avionic display, such as a Vertical Situation Display (VSD), is generated. The controller is configured to: (i) project whether an unstable aircraft state will occur during an approach flown by an aircraft; (ii) when an unstable aircraft state is projected to occur, determine whether implementation of an optimized drag device deployment scheme can prevent the projected occurrence of the unstable aircraft state; and (iii) if determining that the implementation of the optimized drag device deployment scheme can prevent occurrence of the projected unstable aircraft state, generating symbology on the avionic display indicative of the optimized drag device deployment scheme.
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公开(公告)号：US11525699B2
公开(公告)日：2022-12-13
申请号：US16866257
申请日：2020-05-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Akshay Sankeshwari , Sharanabasappa Advani , Bhalakrishnan Janardhanan , Roopa Niveditha Sundara Kulal , Ravish Udupa , Daniel E. Lewis
Abstract: Methods and systems are provided for guiding or otherwise assisting energy management of an aircraft radar vectoring en route to a runway. A method involves determining a predicted lateral trajectory for the radar vectoring in accordance with interception criteria, wherein the lateral trajectory comprises a sequence of segments for satisfying the interception criteria from a current location of the aircraft and each navigational segment of the sequence is associated with an anticipated aircraft heading assignment. The method determines a reference vertical trajectory corresponding to the lateral trajectory, determines a target value for an energy state parameter of the aircraft at the current location on the lateral trajectory using the reference vertical trajectory, and provides indication of a recommended action to reduce a difference between a current value for the energy state parameter and the target value.
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Patent Agency Ranking
6.发明申请公开(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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公开(公告)号：US11682308B2
公开(公告)日：2023-06-20
申请号：US17811938
申请日：2022-07-12
Applicant: Honeywell International Inc.
Inventor： Richard Snyder , Rajeev Mohan , Rajesh Chaubey , Ravish Udupa , Sharanabasappa Advani
CPC classification number: G08G5/0039 , G08G5/006 , G08G5/0013 , G08G5/0021 , G08G5/0026 , 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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公开(公告)号：US20210254997A1
公开(公告)日：2021-08-19
申请号：US16866257
申请日：2020-05-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Akshay Sankeshwari , Sharanabasappa Advani , Bhalakrishnan Janardhanan , Roopa Niveditha Sundara Kulal , Ravish Udupa , Daniel E. Lewis
Abstract: Methods and systems are provided for guiding or otherwise assisting energy management of an aircraft radar vectoring en route to a runway. A method involves determining a predicted lateral trajectory for the radar vectoring in accordance with interception criteria, wherein the lateral trajectory comprises a sequence of segments for satisfying the interception criteria from a current location of the aircraft and each navigational segment of the sequence is associated with an anticipated aircraft heading assignment. The method determines a reference vertical trajectory corresponding to the lateral trajectory, determines a target value for an energy state parameter of the aircraft at the current location on the lateral trajectory using the reference vertical trajectory, and provides indication of a recommended action to reduce a difference between a current value for the energy state parameter and the target value.
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公开(公告)号：US10600328B2
公开(公告)日：2020-03-24
申请号：US15791970
申请日：2017-10-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Sharanabasappa Advani , Rajesh Chaubey
Abstract: An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios. The method includes receiving and processing a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data to determine a an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The method also determines whether an IMC criterion profile and a VMC criterion profile stabilizes the actual approach.
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公开(公告)号：US20190122569A1
公开(公告)日：2019-04-25
申请号：US15791970
申请日：2017-10-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Sharanabasappa Advani , Rajesh Chaubey
IPC: G08G5/02
CPC classification number: G08G5/02 , B64D45/04 , G01C23/00 , G05D1/0676 , G08G5/0021 , G08G5/0026 , G08G5/025
Abstract: An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios is provided. The method includes receiving a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data. These inputs are processed to determine a reference approach profile and an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The approach stabilization criterion is used to determine, whether (a) an IMC criterion profile stabilizes the actual approach and whether (b) a VMC criterion profile stabilizes the actual approach. A display system is commanded to display the approach stabilization criterion; and, when conditions (a) and (b) occur concurrently, user selections responsive to the displayed approach stabilization criterion are processed to update the actual approach profile.
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