An optimization method for target monitoring and tracking performance of airborne collision avoidance system

An airborne anti-collision system and optimization method technology, applied in traffic control systems, aircraft traffic control, instruments, etc., can solve problems such as track interruption, poor angle measurement accuracy, and affect airspace surveillance and situational awareness, and achieve the goal of eliminating The effects of track interruption, maintaining accuracy and stability, and improving situational awareness

Active Publication Date: 2020-09-01
四川九洲空管科技有限责任公司
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AI Technical Summary

Problems solved by technology

The actual situation is that due to the inherent inhomogeneity of the directional antenna pattern, coupled with the fact that after the actual installation, the wing and tail cover the antenna, the blind area of ​​the antenna in the high elevation angle area, and the large maneuvering turn / roll of the carrier aircraft, etc., As a result, the actual angle measurement accuracy often cannot meet the requirements specified in the standard, and the current single target tracking algorithm based on Cartesian filters cannot adapt to antenna occlusion, blind spots, and large maneuvers in actual use, resulting in out-of-tolerance angle measurement accuracy, and even in some cases In this case, it will also cause track interruption, affecting normal airspace surveillance and situational awareness

Method used

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  • An optimization method for target monitoring and tracking performance of airborne collision avoidance system
  • An optimization method for target monitoring and tracking performance of airborne collision avoidance system
  • An optimization method for target monitoring and tracking performance of airborne collision avoidance system

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Embodiment Construction

[0044] The present invention will be further described below in conjunction with the accompanying drawings.

[0045] A method for optimizing the target monitoring and tracking performance of an airborne collision avoidance system, specifically including the following processes:

[0046] (1) According to the heading angle (heading), roll angle (heading), and pitch angle (heading) information input by the aircraft, it is judged whether the aircraft is flying in a large maneuver; if it is, the following process is carried out: according to the evaluation Correct the track angle of the current monitoring and tracking to form a virtual corrected track. According to the azimuth angle of the virtual corrected track, schedule the emission direction of the inquiry signal and make an inquiry; the received response signal meets the track update rule , convert the virtual corrected track into a corrected track and output it to the next processing cycle, and continue during the large maneuve...

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Abstract

The invention relates to the technical field of airborne collision avoidance, and discloses an optimization method for the target monitoring and tracking performance of an airborne collision avoidancesystem. Specifically, the method includes the following processes: judging whether an aircraft is making large maneuvering flight according to the course angle, roll angle and pitch angle informationinput by a carrier aircraft; if the aircraft is making large maneuvering flight, correcting the track angle of current monitoring and tracking according to the evaluated course angle change rate to form a virtual corrected track, and dispatching the launch direction of an inquiry signal according to the azimuth angle of the virtual corrected track to make an inquiry; and if a received response signal satisfies the track updating rule, converting the virtual corrected track into a corrected track and outputting the corrected track to the next processing cycle, and keeping the aircraft in the period of large maneuvering flight. Through the scheme, the influence of the antenna and the installation environment on the azimuth measurement of a target aircraft is eliminated, the accuracy and stability of the track tracking angle are maintained, and the situation awareness ability is improved.

Description

technical field [0001] The invention relates to the technical field of airborne collision avoidance, in particular to a method for optimizing the target monitoring and tracking performance of an airborne anti-collision system. Background technique [0002] Airborne Collision Avoidance System (ACAS-Airborne Collision Avoidance System, also known as TCAS-Traffic Alert and Collision Avoidance System) is defined by the Federal Aviation Administration (FAA). Traffic Alert (TA) and Resolution Alert (RA). TCAS is an essential device to prevent dangerous approaches and collisions of aircraft in the air, and it can work independently of the ground traffic control system. The function and performance index of the system shall meet the minimum performance standard of RTCA / DO185B. The system is mainly used to provide air safety separation guarantee for aircraft, and uses secondary radar to detect approaching aircraft in the nearby airspace. When necessary, it reminds pilots to take ev...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G08G5/00G08G5/04
CPCG08G5/0039G08G5/0078G08G5/045
Inventor 李洪伟付红章学锋卢文韬
Owner 四川九洲空管科技有限责任公司
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