Mixed monitoring tracking method of airborne collision avoidance system

An airborne collision avoidance system and aircraft technology, applied in traffic control systems, aircraft traffic control, instruments, etc., can solve problems such as the loss of conflict detection capabilities, and achieve the effect of reducing the frequency of inquiry and reducing the signal

Inactive Publication Date: 2014-03-26
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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  • Abstract
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AI Technical Summary

Problems solved by technology

ADS-B technology can broadcast various types of monitoring information that is rich in content and meets the requirements of precision and accuracy, but once ADS-B loses the basis for pr

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  • Mixed monitoring tracking method of airborne collision avoidance system
  • Mixed monitoring tracking method of airborne collision avoidance system
  • Mixed monitoring tracking method of airborne collision avoidance system

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Embodiment Construction

[0029] The present invention will be described in further detail below.

[0030] A hybrid monitoring and tracking method for an airborne collision avoidance system, which is based on automatic dependent surveillance-broadcast (ADS-B) technology for passive tracking, and uses the active inquiry of the airborne collision avoidance system (TCAS) itself for active tracking. Switch between monitoring and passive monitoring, replace part of the active monitoring with passive monitoring, reduce the inquiry frequency of the airborne collision avoidance system, increase the monitoring distance of the airborne collision avoidance system, and reduce the signal of inquiry in the airspace. figure 1 It is a block diagram of an airborne collision avoidance system hybrid monitoring and tracking method applied in the airborne collision avoidance system of the present invention. A method for hybrid monitoring and tracking of an airborne collision avoidance system in the present invention is a m...

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Abstract

The invention discloses a mixed monitoring tracking method of an airborne collision avoidance system. According to the method, with a comprehensive use of active monitoring and passive monitoring, mixed monitoring is achieved. The method includes the following steps of: initially using the active monitoring, determining a potential threat condition, tracking and confirming, shifting from the active monitoring to the passive monitoring, verifying passive monitoring data, determining a mixed threat condition, shifting from the passive monitoring to the active monitoring, and tracking and re-confirming. The above operations are used in a certain order to form the mixed monitoring tracking method; with use of the above method, while a collision avoidance capability of an existing TCAS is maintained, the interrogation frequency of the TCAS is reduced, the active request signals in airspace are reduced, and the signal complexity in the airspace is reduced. The ADS-B technology is used, so that the TCAS with the mixed monitoring function is higher in request efficiency, and the TCAS has the capability to track multiple aircrafts.

Description

technical field [0001] The invention relates to air collision avoidance technology, in particular to a monitoring and tracking method in an airborne collision avoidance system. Background technique [0002] TCAS (Traffic Alert and Collision Avoidance System) is an independent air traffic collision avoidance system that provides protection for aircraft equipped with transponders. TCAS actively asks the aircraft equipped with transponders around and tracks the received responses. If the TCAS algorithm determines that the aircraft is invading or is about to intrude, TCAS will issue a traffic alert message (TA); if the intruding aircraft continues to approach, TCAS will issue a decision message ( RA). The protection level provided by TCAS II is determined by the type of transponder carried by the opposing aircraft. If the intruding aircraft reports altitude (C / S mode), TCAS will send out traffic warning information and decision information; if the intruding aircraft is also equ...

Claims

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Application Information

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IPC IPC(8): G08G5/04
Inventor 曹杨华乐斌李杰郑凤马晋缪万胜
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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