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公开(公告)号：US10796589B2
公开(公告)日：2020-10-06
申请号：US15918076
申请日：2018-03-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sriram PR , Steve Cirino , Nathan Shaughn Turner , Jayasenthilnathan B , Satish Narayan Hedge , Sanju Kuriakose , Sreenath Sukumar
Abstract: A method for providing circling approach data onboard an aircraft is disclosed. For a current, circling approach of the aircraft to a destination airport, the method identifies a circling approach procedure applicable to an optimal runway, by a processor communicatively coupled to a system memory element configured to store a database of circling approach procedures and a source for temporary restrictions; determines a circling boundary to the optimal runway, based on the circling approach procedure; determines temporary circling restrictions for the aircraft, based on conflicting traffic from at least a second airport; constructs a lateral path and a vertical path to guide the aircraft to the optimal runway of the destination airport, based on the circling approach procedure, the circling boundary, and the temporary circling restrictions; and presents graphical elements and text associated with the circling approach procedure, the circling boundary, and the temporary restrictions, by a display device.
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公开(公告)号：US20190279516A1
公开(公告)日：2019-09-12
申请号：US15918076
申请日：2018-03-12
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Sriram PR , Steve Cirino , Nathan Shaughn Turner , Jayasenthilnathan B , Satish Narayan Hegde , Sanju Kuriakose , Sreenath Sukumar
Abstract: A method for providing circling approach data onboard an aircraft is disclosed. For a current, circling approach of the aircraft to a destination airport, the method identifies a circling approach procedure applicable to an optimal runway, by a processor communicatively coupled to a system memory element configured to store a database of circling approach procedures and a source for temporary restrictions; determines a circling boundary to the optimal runway, based on the circling approach procedure; determines temporary circling restrictions for the aircraft, based on conflicting traffic from at least a second airport; constructs a lateral path and a vertical path to guide the aircraft to the optimal runway of the destination airport, based on the circling approach procedure, the circling boundary, and the temporary circling restrictions; and presents graphical elements and text associated with the circling approach procedure, the circling boundary, and the temporary restrictions, by a display device.
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