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公开(公告)号：US11587447B2
公开(公告)日：2023-02-21
申请号：US17098561
申请日：2020-11-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Michael Jackson , Ryan Howe-Veenstra
Abstract: Systems and methods provide dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft. The system includes a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path. A control module is coupled to the display system and configured to: demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile; render an RTA speed band graphic having demarked sections vertically representing a speed minimum and speed maximum for an respective RTA speed region, the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region. The control module accepts user modifications and updates the RTA speed band graphic and the current speed profile to reflect user input.
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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.
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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.
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公开(公告)号：US20210233414A1
公开(公告)日：2021-07-29
申请号：US17098561
申请日：2020-11-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sripathi Ramachandra , Michael Jackson , Ryan Howe-Veenstra
IPC: G08G5/00
Abstract: Systems and methods provide dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft. The system includes a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path. A control module is coupled to the display system and configured to: demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile; render an RTA speed band graphic having demarked sections vertically representing a speed minimum and speed maximum for an respective RTA speed region, the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region. The control module accepts user modifications and updates the RTA speed band graphic and the current speed profile to reflect user input.
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