-
公开(公告)号：US20230249842A1
公开(公告)日：2023-08-10
申请号：US17656128
申请日：2022-03-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Gregory Carlucci , Richard Snyder , Michael Jackson , Naresh Bandam , Roopa Niveditha Sundara Kulal , Ambika Sure
Abstract: Methods and systems are provided for assisting operation of a vehicle to satisfy a downpath energy constraint when a current energy state has deviated from a reference energy state according to a planned route of travel. One method involves identifying an intermediate energy constraint at an intermediate point en route to the downpath waypoint, determining a first segment for satisfying the intermediate energy constraint at the intermediate point from the current energy state using a first configuration, determining a second segment from the intermediate point that satisfies the requested energy constraint at the downpath waypoint using a different configuration, and providing graphical indicia of the recommended path including the first and second segments. The graphical indicia includes a first graphical indication of the first configuration associated with the first segment and a second graphical indication of the second configuration associated with the second segment.
-
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.
-
公开(公告)号：US20220139234A1
公开(公告)日：2022-05-05
申请号：US17127504
申请日：2020-12-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Daniel E. Lewis
IPC: G08G5/00
Abstract: Methods and systems are provided for assisting operation of a vehicle deviating from a desired manner of operation, such as an aircraft deviating from a planned trajectory. One method involves identifying a current aircraft altitude, identifying a current aircraft configuration, determining a recommended flight path from the current aircraft altitude for satisfying an upcoming constraint associated with a reference descent strategy based at least in part on the current aircraft configuration in response to a deviation between the current aircraft altitude a target altitude according to the reference descent strategy, and providing an output influenced by the recommended flight path. The recommended flight path includes a recommended vertical profile and a recommended speed profile, and the recommended flight path is configured to vary at least one of a kinetic energy or a potential energy of the aircraft along the recommended flight path en route to the upcoming constraint.
-
公开(公告)号：US11043131B2
公开(公告)日：2021-06-22
申请号：US16285367
申请日：2019-02-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Marek Batelka , Rajesh Chaubey , Jim Rumbo , Kiran Mancheiah Venkataramana , Daniel Corbel , Zdenek Moravek , Ivan Lacko , Zdenek Jancik
Abstract: Provided are enhanced flight guidance systems and methods for an aircraft. The method includes recognizing when the aircraft is in manual operation and an active flight path is different than the planned flight path. An interrupt is received and categorized as one of (i) obstacle, (ii) equipment/fuel, or (iii) pilot health monitor. A managed mode begins, including identifying a rejoining leg of the planned flight path at which to rejoin and a location on the rejoining leg at which to rejoin. A recapture path strategy is selected from (i) lateral, (ii) vertical, and (iii) mixed lateral and vertical. A recapture path to the location on the rejoining leg is computed. The computed recapture path includes speed targets and configuration requirements at dedicated points along the recapture path. Aircraft state data along the recapture path is predicted and guidance controls for the aircraft along the recapture path are generated.
-
公开(公告)号：US20200273349A1
公开(公告)日：2020-08-27
申请号：US16285367
申请日：2019-02-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Marek Batelka , Rajesh Chaubey , Jim Rumbo , Kiran Mancheiah Venkataramana , Daniel Corbel , Zdenek Moravek , Ivan Lacko , Zdenek Jancik
Abstract: Provided are enhanced flight guidance systems and methods for an aircraft. The method includes recognizing when the aircraft is in manual operation and an active flight path is different than the planned flight path. An interrupt is received and categorized as one of (i) obstacle, (ii) equipment/fuel, or (iii) pilot health monitor. A managed mode begins, including identifying a rejoining leg of the planned flight path at which to rejoin and a location on the rejoining leg at which to rejoin. A recapture path strategy is selected from (i) lateral, (ii) vertical, and (iii) mixed lateral and vertical. A recapture path to the location on the rejoining leg is computed. The computed recapture path includes speed targets and configuration requirements at dedicated points along the recapture path. Aircraft state data along the recapture path is predicted and guidance controls for the aircraft along the recapture path are generated.
-
Patent Agency Ranking
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.
-
公开(公告)号：US10026326B1
公开(公告)日：2018-07-17
申请号：US15641525
申请日：2017-07-05
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dorothee De Villele , Rajesh Chaubey , Daniel Corbel , Marek Batelka , Pavel Ptacek
Abstract: Systems and methods directed to generating an adaptive glide slope angle and allowing a pilot to interact with the generated glide slope angle are provided. The systems and methods retrieve, from a navigation database (NDB), a designated approach procedure for the aircraft, and identify a designated glide slope angle (D_GSA) based thereon. The systems and methods receive sensed actual weather data and sensed aircraft status data and generate an adaptive glide slope angle A_GSA based thereon. The systems and methods allow modification of and modify, or prevent modification of, the designated approach procedure with the A_GSA based on the determination of whether or not the A_GSA is compatible with the designated approach procedure.
-
公开(公告)号：US12122530B2
公开(公告)日：2024-10-22
申请号：US17656128
申请日：2022-03-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Gregory Carlucci , Richard Snyder , Michael Jackson , Naresh Bandam , Roopa Niveditha Sundara Kulal , Ambika Sure
Abstract: Methods and systems are provided for assisting operation of a vehicle to satisfy a downpath energy constraint when a current energy state has deviated from a reference energy state according to a planned route of travel. One method involves identifying an intermediate energy constraint at an intermediate point en route to the downpath waypoint, determining a first segment for satisfying the intermediate energy constraint at the intermediate point from the current energy state using a first configuration, determining a second segment from the intermediate point that satisfies the requested energy constraint at the downpath waypoint using a different configuration, and providing graphical indicia of the recommended path including the first and second segments. The graphical indicia includes a first graphical indication of the first configuration associated with the first segment and a second graphical indication of the second configuration associated with the second segment.
-
公开(公告)号：US11842629B2
公开(公告)日：2023-12-12
申请号：US17159608
申请日：2021-01-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rajesh Chaubey , Roopa Niveditha Sundara Kulal , Ambika Sure , Chethan N , Naresh Bandam
CPC classification number: G08G5/025 , G01S13/913 , G08G5/0021
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 dynamically determining an updated predicted lateral trajectory for the radar vectoring when the current aircraft status fails to satisfy a trajectory execution criterion for a previously-predicted lateral trajectory by iteratively adjusting a runway interception point defining a segment aligned with the runway until arriving at the updated predicted lateral trajectory for which a stabilization criterion for the runway can be satisfied. The method determines a target value for an energy state parameter of the aircraft at a current location on the updated predicted lateral 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.
-
20.发明授权公开(公告)号：US11620688B2
公开(公告)日：2023-04-04
申请号：US17303747
申请日：2021-06-07
Applicant: Honeywell International Inc.
Inventor： Rajesh Chaubey , Srihari Jayathirtha , Ivan Markov , Chavdar Kirov
IPC: G06Q30/02 , G06Q30/0283 , G08G5/00
Abstract: A method for providing cost data for a flight is provided. The method (i) obtains cost target data for the flight, under anticipated conditions; (ii) obtains real-time aircraft performance parameters affecting the actual cost of the flight, using continuous monitoring during the flight, including at least aircraft speed modes, aircraft flight level changes, tactical interventions, weather impact, and descent timing deviations; (iii) determines an actual cost of the flight, based on the real-time aircraft performance parameters affecting the actual cost; (iv) identifies flight plan change options associated with a potential cost savings over the actual cost, wherein the flight plan change options comprise potential modifications to the flight plan to complete the flight; (v) presents the flight plan change options; and (vi) adapts operation of one or more avionics systems onboard the aircraft, based on one of the flight plan change options.
-
-
-
-
-
-
-
-
-
Search Results
39
records
(took 0.019 seconds)
