Collision conflict detection method and system

A detection method and target technology, applied in traffic control systems, aircraft traffic control, instruments, etc., can solve problems such as airborne autonomous threat detection and anti-collision enhancement, and achieve the effect of improving airspace flight safety

Active Publication Date: 2018-04-13
四川九洲空管科技有限责任公司
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  • Summary
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The existing airborne collision avoidance system makes limited use of ADS-B information, and cooperates with the secondary radar active interrogation to realize hybrid surveillance, which is used for air-to-air target surveillance at long distances or when there is no threat of collision, which can enhance surveillance stability; at the same time It can reduce the number of active inquiries, thereby reducing space electromagnetic radiation, but the current equipment cannot independently perform threat detection based on ADS-B message information, and generate alarm enhancements
Therefore, for general aviation aircraft, UAVs, helicopters and other aircraft that are not equipped with ACAS equipment, they do not have the capabilities of onboard autonomous threat detection and anti-collision enhancement.

Method used

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  • Collision conflict detection method and system

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specific Embodiment 1

[0034] A collision detection method such as figure 1 Shown is one of the specific embodiments of the present invention. For the ADS-B target near the carrier aircraft, at least two levels of collision conflict areas are established, and according to the motion parameters of the aircraft and the target aircraft, the collision conflict is predicted; Motion parameters include speed, heading and turn rate of own and target aircraft.

[0035] The collision detection method can operate independently of the traditional ACAS system, and predict the collision conflict according to the speed, heading, turning rate and other motion parameters of the own aircraft and the target aircraft.

specific Embodiment 2

[0036] On the basis of the specific embodiment 1, the method further includes, according to the prediction result, if there is a risk of collision, giving a warning prompt, and giving a warning at the same time as the prediction.

specific Embodiment 3

[0037] On the basis of specific embodiment 1 or 2, concrete method steps are:

[0038] Step 1, the ADS-B receiver receives the ADS-B broadcast message in the airspace;

[0039] Step 2, decoding the broadcast message to form the track of the target aircraft and performing track processing to form the track of the target aircraft;

[0040] Step 3, correlating the position, altitude, speed and course information of the target aircraft and the host aircraft, and predicting according to the results of the correlating processing;

[0041]The specific method of predicting in the step 3 is: for each moving target aircraft, with the target aircraft as the center, at least two concentric cylindrical protection spaces are established; wherein, the innermost protection space is called Collision zone; other protection spaces except the collision zone can be called protection zone 1, protection zone 2 and protection zone 3 from inside to outside, and so on; predict whether the carrier airc...

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Abstract

The invention provides a collision conflict detection method and system. The system comprises an ADS-B receiver, an upper / lower omnidirectional antenna, a decoding module, a trajectory processing module and a threat detection module. For an ADS-B target near a host aerial carrier, at least two stages of collision conflict zones are established. Collision conflict is predicted based on the motion parameters of the host aerial carrier and a target aircraft. The motion parameters include speed, the heading and the turn rates of the host aircraft and the target aircraft. Compared with the prior art, collision conflict threat detection can be performed independently based on ADS-B message information. The system can be integrated with ACAS equipment, and can also be independently applied to general aviation aircrafts, unmanned aerial vehicles, and helicopters without ACAS equipment so as to improve flight safety in airspace.

Description

technical field [0001] The invention relates to a collision detection method and system based on the real-time position message of an aircraft, which is suitable for the field of air traffic control collision avoidance. Background technique [0002] Most of the current military and civil aviation aircraft are equipped with airborne collision avoidance systems. The new S-mode transponder realizes the air traffic control response function and also has the ADS-B OUT function, which can broadcast the flight ID, real-time position, and altitude of the aircraft to other aircraft in real time. information. The following is an introduction to the functions of the airborne collision avoidance system and ADS-B. [0003] Airborne Collision Avoidance System (ACAS: Airborne Collision Avoidance System) has been in existence for more than 30 years. It is defined by the Federal Aviation Administration (FAA) and is an essential device to prevent dangerous approach and collision accidents of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/04
CPCG08G5/04
Inventor 李洪伟刘杰才李家蓬
Owner 四川九洲空管科技有限责任公司
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