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公开(公告)号:US20220196783A1
公开(公告)日:2022-06-23
申请号:US17127526
申请日:2020-12-18
Applicant: Zebra Technologies Corporation
Inventor: Thomas Dorris , Adam Imran
Abstract: A non-transitory computer-readable medium storing a plurality of computer-readable instructions executable by a processor, wherein execution of the instructions configures the processor to: obtain location data representing a ground path of a flight of an object; determine, from the location data, a first ground distance and a second ground distance traversed by the object during an ascent phase and a descent phase of the flight of the object, respectively; determine an initial angle of the flight of the object; determine an initial airspeed of the object based on the determined initial angle; determine an air drag value for the object during the flight based on the determined initial angle and the determined initial airspeed; output a flight path of the object, the flight path representing a three-dimensional path travelled by the object during the flight and determined based on the initial angle, the initial airspeed and the air drag value.
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公开(公告)号:US11927686B2
公开(公告)日:2024-03-12
申请号:US17127526
申请日:2020-12-18
Applicant: Zebra Technologies Corporation
Inventor: Thomas Dorris , Adam Imran
CPC classification number: G01S5/0294 , A63B24/0021 , G01S5/06 , G06T17/00 , A63B2024/0034 , A63B2220/62 , A63B2220/833 , A63B2225/54 , A63B2243/007
Abstract: A non-transitory computer-readable medium storing a plurality of computer-readable instructions executable by a processor, wherein execution of the instructions configures the processor to: obtain location data representing a ground path of a flight of an object; determine, from the location data, a first ground distance and a second ground distance traversed by the object during an ascent phase and a descent phase of the flight of the object, respectively; determine an initial angle of the flight of the object; determine an initial airspeed of the object based on the determined initial angle; determine an air drag value for the object during the flight based on the determined initial angle and the determined initial airspeed; output a flight path of the object, the flight path representing a three-dimensional path travelled by the object during the flight and determined based on the initial angle, the initial airspeed and the air drag value.
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