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Radar dynamic target calibration method and system based on eye-movement tracking

A dynamic target and eye-tracking technology, applied in traffic control systems, data processing input/output process, user/computer interaction input/output, etc., can solve the problem of low efficiency, affecting the timeliness and reliability of aircraft command and deployment , Inapplicable airspace environment and other issues, to achieve the effect of solving inapplicability, improving timeliness and reliability, and improving calibration efficiency

Active Publication Date: 2019-07-19
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology

[0003] At present, air traffic controllers use manual calibration to calibrate the dynamic target area. The manual calibration method is inefficient, affects the timeliness and reliability of aircraft command and deployment, and is not suitable for the current complex airspace environment.

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  • Radar dynamic target calibration method and system based on eye-movement tracking
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Embodiment Construction

[0048] In order to make the purpose, features and advantages of the present invention more obvious and understandable, the technical solutions protected by the present invention will be clearly and completely described below using specific embodiments and accompanying drawings. Obviously, the implementation described below Examples are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in this patent, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this patent.

[0049] This embodiment provides a radar dynamic target calibration method based on eye tracking, which monitors the controller's eye physiological parameters in real time, fits the eye measurement data with the real-time position information of the aircraft, calibrates the dynamic target on the radar screen, and identifies the controller Pay attention to the allocation of resources, which ...

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Abstract

The invention provides a radar dynamic target calibration method and system based on eye-movement tracking. The radar dynamic target calibration method comprises the steps that real-time geographicalcoordinate data of an aircraft and screen coordinate data in a radar interface are obtained; eye-movement fixation point data are obtained, and a fixation point static area is calibrated in the radarinterface; and a geographical coordinate and screen coordinate conversion model is established, and a dynamic target area is calibrated according to the conversion model. Eye physiological parametersof a controller are monitored in real time, eye measuring data are fitted with real-time position information of the aircraft, a dynamic target in a radar screen is calibrated, distribution of controller attention resources is identified, and the timeliness and reliability of commanding and deploying the aircraft are improved.

Description

technical field [0001] The invention relates to the field of air traffic control, in particular to a radar dynamic target marking method and system based on eye movement tracking. Background technique [0002] As an important position in the air traffic management system, the controller plays a vital role in the reliability, safety and efficiency of the aircraft. With the rapid development of air transport, the number of aircraft in the airspace has increased sharply, forming a complex airspace environment. The work pressure and workload of air traffic controllers are increasing day by day. The range of gaze transfer of controllers will be reduced due to the increase in the complexity of the airspace environment. It is very likely that gaze transfer and search information will only be performed between some aircraft, thereby improving attention resources. Unreasonable distribution. Therefore, it is of great practical significance to accurately identify and extract the spec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/00G06F3/01
CPCG06F3/013G08G5/0082
Inventor 靳慧斌胡占尧霍百明常银霞
Owner CIVIL AVIATION UNIV OF CHINA
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