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1.
公开(公告)号:US20210009281A1
公开(公告)日:2021-01-14
申请号:US16504956
申请日:2019-07-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zuowei He , Thea Feyereisen , Gang He , Ye He
Abstract: Methods and systems are provided for adjusting a dynamic scale indicator on a flight display of an aircraft. The method comprises receiving an operational status parameter for the aircraft and generating the dynamic scale indicator located on the flight display of the aircraft. The dynamic scale indicator includes a positive value range that represents operational status parameter values greater than a selected setting value and a negative value range that represents operational status parameter values less than the selected setting value. The operational status parameter is translated into a value that is represented on the dynamic scale indicator. The value ranges shown on the dynamic scale indicator are adjusted by fading the negative value range when the operational status parameter value is positive, fading the positive value range when the operational status parameter value is negative, and fading the value range to the extent that the value range exceeds the operational status parameter value.
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公开(公告)号:US20240355214A1
公开(公告)日:2024-10-24
申请号:US18302367
申请日:2023-04-18
Applicant: HONEYWELL INTERNATIONAL INC.
CPC classification number: G08G5/0078 , B64D43/00 , B64D47/08 , G08G5/0021 , H04N7/185 , G01C23/00
Abstract: Systems and methods are provided for in-air traffic tracking onboard an ownship. The system includes a display device, a sensor system configured to sense a sensed three-dimensional (3D) position of a target aircraft, a communication system configured to receive in-air traffic position data from an external source that includes a tracked 3D position of the target aircraft, and an in-air traffic tracking system that includes a controller configured to, by a processor: determine a predicted 3D position of the target aircraft by adjusting the tracked 3D position with compensation parameters, wherein the compensation parameters are determined based on a trained machine learning, determine a real-time 3D position of the target aircraft based on the sensed 3D position and/or the predicted 3D position, and render a tracking icon on the display device that indicates the real-time 3D position of the target aircraft.
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