公开(公告)号：US10699584B2

公开(公告)日：2020-06-30

申请号：US15910072

申请日：2018-03-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： John G. Suddreth ,  Jerry Ball ,  Troy Nichols ,  Mark A. Giddings

IPC: G08G5/00 ,  G01C23/00 ,  B64C30/00

Abstract: Flight planning systems and methods are provided, which augment supersonic flight planning via the integration of sonic boom forecast data. In embodiments, the flight planning system includes a display device, a pilot input interface, and a controller architecture coupled to the display device and to the pilot input interface. During system operation, the controller architecture receives flight plan criteria entered via the pilot input interface. The controller architecture then endeavors to generate or construct a boom-regulated flight plan, which includes at least one supersonic flight plan segment, in accordance with the flight plan criteria. If unable to construct a boom-regulated flight plan, the controller architecture generates a visual notification on the display device. The visual notification can include, for example, a warning that an excessive sonic boom or overpressure event may occur during execution of the flight plan by an aircraft, absent modifications to the flight plan.

公开(公告)号：US20190272762A1

公开(公告)日：2019-09-05

申请号：US15910072

申请日：2018-03-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： John G. Suddreth ,  Jerry Ball ,  Troy Nichols ,  Mark A. Giddings

IPC: G08G5/00

Abstract: Flight planning systems and methods are provided, which augment supersonic flight planning via the integration of sonic boom forecast data. In embodiments, the flight planning system includes a display device, a pilot input interface, and a controller architecture coupled to the display device and to the pilot input interface. During system operation, the controller architecture receives flight plan criteria entered via the pilot input interface. The controller architecture then endeavors to generate or construct a boom-regulated flight plan, which includes at least one supersonic flight plan segment, in accordance with the flight plan criteria. If unable to construct a boom-regulated flight plan, the controller architecture generates a visual notification on the display device. The visual notification can include, for example, a warning that an excessive sonic boom or overpressure event may occur during execution of the flight plan by an aircraft, absent modifications to the flight plan.