KR20110095637A - Anticollision communication system of an aircraft - Google Patents

Abstract

PURPOSE: An anti-collision communication system of an aircraft is provided to implement the anti-collision with a manned aircraft by enabling an unmanned aircraft to collect the information of the manned aircraft. CONSTITUTION: In an anti-collision communication system of an aircraft, a manned aircraft has a communications system. The communications system comprises a transponder, a communications control module, and a traffic database. An unmanned aircraft has a communications system. The communications system includes a UAV interrogator, a UAV communication unit, a UAV communications control module, and a UAV flight information database. The UAV interrogator is comprised of a transmission unit, a receiver, and a decoder. A GCS has a communications system including a GCS communications unit, a GCS communications control module, a GCS flight information database, and a pilot manipulator.

Description

Anti-collision communication system {Anticollision communication system of an aircraft}

The present invention relates to a communication system for collision prevention between manned-unmanned aircraft or unmanned-unmanned aircraft,

In the manned-unmanned aircraft communication system, SSR Sytem composed of a transponder consisting of a question receiver and a responder, and an interrogator composed of a transmitter, a receiver and a decoder; A communication control module; A manned aircraft having a communication system including a communication database; A UAV interrogator composed of a transmitter, a receiver and a decoder interoperable with a transponder of the manned aircraft, a UAV-SSR Sytem composed of a UAV transponder composed of a question receiver and an interoperator interoperable with an interrogator of the manned aircraft ; A UAV communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with a GCS communication transmitter-receiver of the GCS; UAV communication control module; An unmanned aerial vehicle (UAV) having a communication system including a UAV flight information database; A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle; A GCS communication control module; A GCS flight information database; A GCS having a communication system comprising a pilot manipulator; The communication system of the manned aircraft and the unmanned aerial vehicle is interoperable with each other to exchange predetermined information;

In the unmanned-unmanned aircraft communication system, using the unmanned aerial vehicle communication system of the manned-unmanned aerial vehicle communication system of the unmanned-unmanned aircraft interoperable with each other characterized in that the predetermined information exchange is possible The field of collision avoidance communication systems between unmanned aircraft or unmanned aerial vehicles.

With the development of the aviation industry, the modern society is continuously increasing supply and demand for manned and unmanned aircraft. Accordingly, the aircraft flight area regulation and air traffic control system that can manage the flight of the aircraft are being researched and developed in various fields. The conventional manned aircraft and the ground control station are the primary surveillance radar (PSR), as shown in FIG. Secondary Surveillance Radar (SSR) and voice communication were used to communicate information to manned aircraft and ground control stations. In detail, in terms of the ground control station, the manned aircraft operating in the flight route through the primary monitor configured in the ground control station is managed within the scope of the monitoring station, and the secondary surveillance radar (SSR) is used. The manned aircraft located farther than the primary surveillance radar could be identified and identified to induce safer takeoff and landing. However, despite the air traffic control system as described above, there is a problem that a detailed system for collision avoidance has not been presented in the inter-flight of manned-unmanned aircraft or unmanned-unmanned aircraft.

Looking at the prior art associated with the above is as follows. That is, Korean Laid-Open Patent Publication No. 10-2008-0113021 relates to an aircraft collision detection / avoidance system and method, wherein the collision detection / avoidance system identifies potential collision risks for an aircraft to avoid any identified risk. An image interrogator to provide activation; Motion sensors (such as imaging and / or infrared sensors) provide cluttersuppression and target detection devices for detecting local targets moving within the frame around image frames; Line of sight (LOS), the multi-target tracking device tracks the detected local target and maintains a tracking history in LOS coordinates for each detected local target; The risk assessment apparatus determines which tracked local targets involve a collision risk; The evasion starting device is configured to provide flight control and guidance devices with a maneuver for avoiding any identified collision risks, and has tried to prevent the collision of the aircraft. See-avoid 'system is only applied to the mechanical system, and the collision avoidance function is prevented when the image providing and motion sensor fail to perform its original function due to cloudy weather or poor air condition. There is a problem that can not be carried out, the continuous research and development of the communication system to prevent the collision of the aircraft is required.

The present invention has been made to improve the problems according to the communication system for preventing collision between manned-unmanned aircraft or unmanned-unmanned aircraft,

Conventional aircraft communication system has a problem that the collision accident of the aircraft may occur because there is no specific communication system between the manned aircraft and the unmanned aerial vehicle or unmanned aerial vehicle and unmanned aerial vehicle; In order to solve the above problems, the flight route of manned aircraft is systematically prohibited from flying an unmanned aerial vehicle, or a certain flightable area is allocated only for a certain time so that the flight of the unmanned aerial vehicle does not affect the flying of the manned aircraft. It aims to provide a solution to the problem of limiting the flight of unmanned aerial vehicles.

The present invention is to realize the desired object as described above,

In the manned-unmanned aircraft communication system, SSR Sytem composed of a transponder consisting of a question receiver and a responder, and an interrogator composed of a transmitter, a receiver and a decoder; A communication control module; A manned aircraft having a communication system including a communication database; A UAV interrogator comprising a transmitter, a receiver and a decoder interoperable with a transponder of the manned aircraft, a UAV-SSR Sytem composed of a UAV transponder composed of a question receiver and an interoperator interoperable with an interrogator of the manned aircraft ; A UAV communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with a GCS communication transmitter-receiver of the GCS; UAV communication control module; An unmanned aerial vehicle having a communication system including a UAV flight information database; A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle; A GCS communication control module; A GCS flight information database; A GCS having a communication system comprising a pilot manipulator; Communication systems of the manned and unmanned aerial vehicles are interoperable with each other to exchange predetermined information;

In the unmanned-unmanned aircraft communication system, using the unmanned aerial vehicle communication system of the manned-unmanned aerial vehicle communication system of the unmanned-unmanned aircraft interoperable with each other characterized in that the predetermined information exchange is possible -Propose an anti-collision communication system between an unmanned aircraft or an unmanned aerial vehicle.

The communication system for preventing collision between the manned-unmanned aircraft or the unmanned-unmanned aircraft according to the present invention, as a means for solving the above problems, constitutes a UAV interrogator capable of communicating with a manned aircraft in an unmanned aerial vehicle, the unmanned aerial vehicle in the configuration Obtaining the manned aircraft information to enable collision avoidance with the manned aircraft; In connection with the above, the UAV transponder may be further configured to include an intergate in a manned aircraft configured only with a conventional transponder, and the UAV transponder may be avoided by an unmanned aerial vehicle. In addition, the manned aircraft can avoid the adjacent unmanned aerial vehicle, and it is possible to communicate with the ground control station and the unmanned aerial vehicle so that the drone pilot can easily receive the flight control instruction of the control station. In addition, it is also possible to obtain an effect of preventing a collision between the unmanned aerial vehicle and the unmanned aerial vehicle by using the communication system of the unmanned aerial vehicle having the above configuration. Furthermore, the present invention is an unmanned aerial vehicle industry, which is the next-generation cutting-edge growth engine industry by improving the use of complex air spaces and contributing to aviation safety, and solving the problem of entering the private airspace, which is the biggest challenge of the activation of the unmanned aerial vehicle industry. Has an activating effect.

1 is a schematic diagram showing a conventional aircraft communication system.
2 is a schematic diagram showing an anti-collision communication system between a manned and unmanned aerial vehicle according to a preferred embodiment of the present invention.
3 is a block diagram of an aircraft collision avoidance communication system between a manned and unmanned aircraft of a preferred embodiment of the present invention.
4 is a block diagram of an anti-collision communication system between a manned and unmanned aerial vehicle according to another preferred embodiment of the present invention.
5 is a schematic diagram showing an anti-collision communication system between an unmanned aerial vehicle and an unmanned aerial vehicle according to a preferred embodiment of the present invention.
Figure 6 is a block diagram of an aircraft collision avoidance communication system between the unmanned and unmanned aircraft of the preferred embodiment of the present invention.

The present invention relates to a communication system for preventing collision between manned and unmanned aerial vehicle, comprising: a transponder composed of a question receiver and a responder, and an SSR sytem composed of an interrogator composed of a transmitter, a receiver, and a decoder; A communication control module; A manned aircraft 30 having a communication system including a communication database; It consists of a UAV interrogator composed of a transmitter, a receiver and a decoder interoperable with the transponder of the manned aircraft 30, and a UAV transponder composed of a question receiver and a responder interoperable with the interrogator of the manned aircraft 30. UAV-SSR Sytem; A UAV communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with a GCS communication transmitter-receiver of a ground control system (hereinafter referred to as GCS 20); UAV communication control module; An unmanned aerial vehicle 10 having a communication system including a UAV flight information database; A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle 10; A GCS communication control module; A GCS flight information database; A GCS 20 having a communication system comprising a pilot manipulator; The communication system of the manned aircraft 30 and the unmanned aerial vehicle 10 can interoperate with each other to exchange predetermined information; In the communication system of the unmanned-unmanned aircraft, by using the communication system of the unmanned aerial vehicle 10 of the manned-unmanned aerial vehicle communication system, the communication system of the unmanned-unmanned aircraft is interoperable with each other, so that predetermined information exchange is possible. An anti-collision communication system between a manned-unmanned aircraft or an unmanned-unmanned aircraft.

Hereinafter, the present invention will be described in detail with reference to the accompanying drawings 1 to 6 showing an embodiment to which the present invention is applied.

First, the manned aircraft 30 'and the ground control station 40' include a primary surveillance radar (PSR) and a secondary surveillance radar (SSR) as shown in FIG. And a communication system to exchange information between the manned aircraft 30 'and the ground control station 40' through voice communication. Looking at this in more detail in terms of the ground control station 40 ', the manned aircraft 30' operating in the flight route is managed within the scope of the supervisor via the PSR system configured in the ground control station 40 ', and the SSR system is used. It is a communication method that finds and identifies manned aircraft 30 'located farther than the PSR system and uses it for safer takeoff and landing during takeoff and landing of manned aircraft 30'. The communication system between the manned aircraft 30 'and the ground control station 40' using the PSR system and the SSR system described above did not cause problems in the mutual communication between the manned aircraft 30 'and the ground control station 40'. Communication with the unmanned aerial vehicle 30 'and the unmanned aerial vehicle 10 "or the unmanned aerial vehicle 10" or the ground control station 40' in communication with the unmanned aerial vehicle 10 "for civil or military purposes is difficult. 30 ') and a collision between the unmanned aerial vehicle 10 "occur. In addition, conventionally, in order to solve the above problems, the unmanned aerial vehicle 10 'is not allowed to fly in the flight path of the manned aircraft 30', or the unmanned aerial vehicle 10 'is not allowed to fly. There was a problem in that the flight of the unmanned aerial vehicle 10 "should be restricted in such a manner as to allocate a certain flightable area only for a predetermined time so as not to affect the flight of the aircraft.

On the other hand, the present invention configures a UAV interrogator capable of communicating with the manned aircraft 30 in the unmanned aerial vehicle 10 to solve the above problems, and the unmanned aerial vehicle 10 obtains the manned aircraft information by the above configuration. Inventions that enable collision avoidance with the aircraft 30 have been made (Example 1); In connection with the above, the unmanned aerial vehicle 10 may be configured to further include an intergate in the manned aircraft 30 including only the conventional transponder, and further configure a UAV transponder together with the UAV interrogator in the unmanned aerial vehicle 10. Not only can avoid the close manned aircraft 30, but also the manned aircraft 30 can also avoid the close unmanned aerial vehicle 10, enabling the communication between the unmanned aerial vehicle 10 and the ground control station 40 unmanned. Aircraft 10 pilots invented the invention (Example 2) to be more easily received the flight control instruction of the ground control station 40; When the unmanned aerial vehicle 10 constituting the second embodiment has a plurality of flight operations, communication between the unmanned aerial vehicle and the unmanned aerial vehicle is also possible to prevent collision between the unmanned aerial vehicle and the unmanned aerial vehicle (Example 3). Hereinafter is a preferred embodiment of the aircraft collision avoidance communication system according to the present invention.

Example 1

The present invention provides a transponder comprising a question receiver and an answering machine: a communication control module; A manned aircraft 30 having a communication system including a communication database; A UAV interrogator comprising a transmitter, a receiver, and a decoder interoperable with a transponder of the manned aircraft communication system, comprising: a main communication transmitter-receiver and a preliminary communication transmitter-receiver that are interoperable with a GCS communication transmitter-receiver of the following GCS. A UAV communication transmitter-receiver; UAV communication control module; An unmanned aerial vehicle 10 having a communication system including a UAV flight information database; A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle 10; A GCS communication control module; A GCS flight information database; A GCS 20 having a communication system comprising a pilot manipulator; By configuring the communication system of the manned aircraft 30 and the unmanned aerial vehicle 10 so as to be interoperable with each other to exchange predetermined information, predetermined identification information and operation information (altitude, speed, etc.) of each manned aircraft 30 are provided. (Hereinafter, the manned aircraft information) can be obtained by the unmanned aerial vehicle 10, and the unmanned aerial vehicle 10 can be obtained from the unmanned aerial vehicle 10 through communication between the unmanned aerial vehicle 10 and the GCS 20. Since the pilot is recognizable, the unmanned aerial vehicle 10 may adjust the unmanned aerial vehicle 10 by using the manned aircraft information obtained by the pilot, thereby preventing collision between the manned aerial vehicle 30 and the unmanned aerial vehicle 10.

That is, the UAV interrogator of the unmanned aerial vehicle 10, which is the main configuration of the present invention, uses the UAV communication control module to send a predetermined question data included in the UAV flight information database to the manned aircraft 30 around the unmanned aerial vehicle 10. The manned aircraft 30, which receives the question data to the question receiver of the transponder, sends out the manned aircraft information as a responder and provides it to the receiver of the UAV interface; The unmanned aerial vehicle 10 receiving the manned aircraft information interprets the manned aircraft information by using a decoder and transmits it to the UAV communication control module, and the UAV communication control module receiving the manned aircraft information is a UAV communication transmission / reception unit (C-band). UAV pilots transmit the manned aircraft information to the UCS communication control module associated with the GCS communication sender / receiver by transmitting the manned aircraft information to the GCS communication sender / receiver (C-band receiver) of the GCS 20 through a transmitter. The UAV pilot, which has been made recognizable and recognizes the manned aircraft information through the above process, adjusts the unmanned aerial vehicle 10 to avoid the range of the flight area that may interfere with the flight of the manned aircraft 30. There is an effect that can prevent the collision with the unmanned aerial vehicle (10).

At this time, the communication between the unmanned aerial vehicle 10 and the GCS 20 has a main communication transmitter and receiver using C-band (radio waves having a radar frequency band of 4 to 8 GHz) and a UHF (radar frequency band of 300 MHz to 3 GHz). Preliminary communication using radio waves) The main communication using the C-band is used for the purpose of exchanging main information on the control and communication of the unmanned aerial vehicle, and the preliminary communication using the UHF is an unmanned aerial vehicle (10). The purpose of this is to transmit and receive the image information taken by the user or preliminary communication when the main communication is disconnected.

In addition, the present invention is configured so that the UAV flight information database, which is the communication system configuration of the unmanned aerial vehicle 10, further includes an anti-collision automatic control processing data, the communication between the manned aircraft 30 and the unmanned aerial vehicle 10 having the above configuration. If the unmanned aerial vehicle 10 obtained the information of the manned aircraft through the system encounters a collision risk with the manned aircraft 30 without the pilot command of the unmanned aerial vehicle 10, the collision with the manned aircraft 30 may be avoided by itself. It is possible to configure. That is, since the conventional unmanned aerial vehicle 10 "has only flight information of the unmanned aerial vehicle 10" itself generated using only the configuration of a satellite sensor (GPS), an inertial sensor, an inertial value calculation module, a position estimation module, and the like, Although it is difficult to obtain flight information (positional information and speed information) of a collision dangerous object such as an aircraft 30 ', the risk of collision with the manned aircraft 30' can be avoided only by the judgment of the unmanned aerial vehicle 10 '. In the aircraft communication system according to the present invention, the UAV communication control of the unmanned aerial vehicle 10 is possible because the unmanned aerial vehicle 10 can obtain not only flight information of the unmanned aerial vehicle 10 itself but also manned aircraft information around the unmanned aerial vehicle 10. The module can control the unmanned aerial vehicle 10 to avoid collision with the unmanned aerial vehicle 30 by itself using the collision avoidance automatic control processing data included in the UAV flight information database. In detail, the collision of the unmanned aerial vehicle 10 with the manned aircraft 30 has occurred, but the situation where the unmanned aerial vehicle 10 is not recognized due to a mistake of the pilot of the unmanned aerial vehicle 10 or the communication between the unmanned aerial vehicle 10 and the GCS 20 When a disconnected situation occurs and a situation in which the manned aircraft 30 and the unmanned aerial vehicle 10 may collide, the UAV communication control module of the unmanned aerial vehicle 10 uses the manned aircraft information obtained by using the manned aircraft information obtained through the UAV interrogator. Produces prediction information for predicting the altitude and speed of (30), and the UAV communication control module automatically controls the speed of the unmanned aerial vehicle 10 by using the generated prediction information (increases or decreases the speed) Manned aviation by controlling the unmanned aerial vehicle 10 using a method or an automatic control process (which raises or lowers altitude) to maintain a constant altitude difference with the manned aircraft 30). You can achieve the effect that you can avoid the risk of collision with (30).

In addition, the present invention includes a UAV information data including a plurality of UAV identification information (unique code assigned by authenticating each unmanned aerial vehicle) communication database of the manned aircraft 30, the communication control module of the manned aircraft 30 is The UAV identification information is used to transmit the manned aircraft information only to the UAV included in the UAV information data through the transponder's responder, thereby preventing the provision of the manned aircraft information requiring confidentiality to the unmanned unmanned aerial vehicle 10. You can get the effect. That is, since the manned aircraft 30 flight information (manned aircraft information) needs to be kept confidential for the safety of flight of the manned aircraft 30, the collision prevention between the manned aircraft 30 and the unmanned aerial vehicle 10 according to the present invention is prevented. This is because if the communication for the indiscriminately made can cause a serious problem on the safety of the manned aircraft (30).

[Example 2]

The present invention further includes an interrogator consisting of a transmitter, a receiver, and a decoder such that the manned aircraft communication system includes a configuration of the first embodiment so that an integrated SSR system is configured together with a transponder; The unmanned aerial vehicle 10 communication system further includes a UAV transponder including a question receiver and an interoperator interoperable with the interrogator of the manned aircraft communication system, so that the UAV interrogator and the UAV-SSR Sytem are configured. Not only the unmanned aerial vehicle 10 can obtain the manned aircraft information, but also the manned aerial vehicle 30 can also obtain certain identification information and operation information (altitude, speed, etc.) of the unmanned aerial vehicle 10 (hereinafter, referred to as unmanned aerial vehicle information). It can be done.

This embodiment 1 is a collision avoidance that can avoid the collision risk by flying the unmanned aerial vehicle 10, the speed and size smaller than the manned aircraft 30 to avoid the manned aircraft 30, when the collision risk occurs While the communication system is embodied, the present embodiment 2 is configured such that the manned aircraft 30 also obtains unmanned aerial vehicle information close to the manned aircraft 30 to avoid a collision risk.

That is, the interrogator configured in the manned aircraft 30 transmits the question data of the schedule included in the communication database to the unmanned aerial vehicle 10 around the manned aircraft 30 by the communication control module, and transmits the question data. The unmanned aerial vehicle 10 received by the question receiving unit of the transponder transmits the unmanned aerial vehicle information as a responder and provides it to the receiving unit of the manned aircraft 30 intergate; The unmanned aerial vehicle 30 receiving the unmanned aerial vehicle information interprets the unmanned aerial vehicle information using a decoder and transmits the unmanned aerial vehicle information to the communication control module, and the unmanned aerial vehicle information is transmitted to the pilot UI through the communication control module so that the manned aircraft 30 pilot An effect of recognizing the unmanned aerial vehicle information can be obtained. This enables the pilot of the manned aircraft 30 to recognize the information of the unmanned aircraft around the flight route of the manned aircraft 30, thereby making itself possible to avoid the collision risk between the manned aircraft 30 and the unmanned aerial vehicle 10, and furthermore, the manned aircraft in flight. The warning about the unmanned aerial vehicle 10 causing the collision risk to the aircraft 30 is transmitted to the ground control station 40, and the ground control station 40 can be quickly delivered to the pilot of the unmanned aerial vehicle 10 so that the manned aircraft ( 30) and the collision risk between the unmanned aerial vehicle 10 can be obtained double.

In addition, the above configuration has the effect that the unmanned aerial vehicle 10 can respond as a UAV transponder to the question signal sent from the transmitter of the ground control station 40 inter-gate configured in the ground control station 40 and the unmanned aerial vehicle 10 and It is possible to communicate with the ground control station 40, and if the collision with the manned aircraft due to the abnormal flight of the unmanned aerial vehicle 10, the effect of enabling a prompt flight control instruction to the unmanned aerial vehicle pilot at the ground control station 40 Can also be obtained.

Example 3

In addition, the present invention can also obtain the effect of preventing the collision between the unmanned-unmanned aerial vehicle when the unmanned aerial vehicle 10 and the GCS 20 configured in the second embodiment a plurality of flights.

That is, the present invention provides a UAV transponder composed of a question receiver and a responder, and a UAV-SSR Sytem composed of a UAV interrogator composed of a transmitter, a receiver, and a decoder; A UAV communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with a GCS communication transmitter-receiver of the GCS; UAV communication control module; An unmanned aerial vehicle 10 having a communication system including a UAV flight information database; A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle 10; A GCS communication control module; A GCS flight information database; A GCS 20 having a communication system comprising a pilot manipulator; When the unmanned aerial vehicle 10 and the GCS 20 having the above configuration are operated in plural flights, the communication system of the unmanned aerial vehicle 10 and the other unmanned aerial vehicle 10 'is interoperable with each other so that predetermined information exchange is possible. Thus, as shown in FIGS. 5 to 6, UAV-SSR composed of UAV transponders and UAV interrogators of unmanned aerial vehicle 10 and exchange of unmanned aerial vehicle information between the unmanned aerial vehicle 10 and other unmanned aerial vehicle 10 'is possible. The intercommunication between the Sytem and the UAV-SSR Sytem 'constituted by the UAV transponder' and the UAV interrogator 'of the other unmanned aerial vehicle 10' is the mutual communication between the manned aircraft 30 and the unmanned aerial vehicle 10 of the second embodiment. Equal to; GAV communication transmission consisting of UAV communication transmission / reception section composed of main communication transmission / reception section and preliminary communication transmission / reception section of other unmanned aerial vehicle 10 'and main communication transmission / reception section, and preliminary communication transmission / reception section. The mutual communication between the receivers is also made on the same principle as the mutual communication between the unmanned aerial vehicle 10 and the GCS 20 of the second embodiment.

In addition, in order to prevent a collision between the unmanned aerial vehicle 10 and another unmanned aerial vehicle 10 ', the UAV flight information database of the unmanned aerial vehicle 10, like the unmanned aerial vehicle 10 of Embodiment 1, is automatically controlled to prevent collisions. Further includes data; The UAV communication control module of the unmanned aerial vehicle 10 generates prediction information for predicting the altitude and speed of another unmanned aerial vehicle 10 by using the unmanned aerial vehicle information of another unmanned aerial vehicle 10 'obtained through the UAV interrogator. The UAV communication control module automatically controls the speed of the unmanned aerial vehicle 10 itself using the generated prediction information, and automatically controls the altitude so as to maintain a constant altitude difference with the other unmanned aerial vehicle 10 '. The above-described automatic control process can be configured to avoid the risk of collision with another unmanned aerial vehicle 10 ', thereby preventing the collision between the unmanned aerial vehicle and the unmanned aerial vehicle.

In addition, in the present invention, the UAV flight information database of the unmanned aerial vehicle 10 includes unique UAV identification information of the unmanned aerial vehicle 10; The UAV communication database 'of the other unmanned aerial vehicle 10' includes UAV information data containing a plurality of UAV unique UAV identification information; The communication control module of the other unmanned aerial vehicle 10 'uses only the unmanned aerial vehicle 10 included in the UAV information data using the unique UAV identification information of the unmanned aerial vehicle 10 through the transponder's answering machine. 10 ') to send the unmanned aerial vehicle information', the manned aerial vehicle 30 of the first embodiment provides the manned aerial vehicle information only to the certified unmanned aerial vehicle 10 (unmanned aerial vehicle having a unique code) to the manned aerial vehicle 30 It is possible to obtain the effect of maintaining the security of the unmanned aerial vehicle 10 that requires the plane, such as a military unmanned aerial vehicle to maintain the flight safety of the.

The above has been described with reference to a preferred embodiment of the present invention, the present invention is not limited to the above embodiments, those skilled in the art to which the present invention pertains through the above embodiments the gist of the present invention Various changes can be made without departing.

10: unmanned aerial vehicle 20: GCS
30: manned aircraft 40: ground control station

Claims (7)

A transponder comprising a question receiver and a responder: a communication control module; A manned aircraft 30 having a communication system including a communication database;
A UAV interrogator comprising a transmitter, a receiver, and a decoder interoperable with a transponder of the manned aircraft communication system, comprising: a main communication transmitter-receiver and a preliminary communication transmitter-receiver that are interoperable with a GCS communication transmitter-receiver of the following GCS. A UAV communication transmitter-receiver; UAV communication control module; An unmanned aerial vehicle 10 having a communication system including a UAV flight information database;
A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle 10; A GCS communication control module; A GCS flight information database; A GCS 20 having a communication system comprising a pilot manipulator;
The manned-unmanned aircraft collision prevention communication system, characterized in that the communication system of the manned aircraft (30) and the unmanned aerial vehicle (10) can be interoperable with each other.
The method of claim 1,
The manned aircraft communication system further includes an interrogator including a transmitter, a receiver, and a decoder, in which an SSR system is configured together with a transponder;
The unmanned aerial vehicle 10 communication system further includes a UAV transponder including a question receiver and an answering device interoperable with the interrogator of the manned aircraft communication system. A manned-unmanned aerial vehicle collision prevention communication system, characterized in that.
The method of claim 1,
The UAV flight information database further includes anti-collision automatic control processing data,
The UAV communication control module of the unmanned aerial vehicle 10 generates prediction information for predicting the altitude and speed of the manned aircraft 30 by using the manned aircraft information obtained through the UAV interrogator, and the UAV communication control module generates the UAV communication control module. By using the predicted information, one or more of the automatic control process of the automatic control processing of the speed of the unmanned aerial vehicle 10 itself, the automatic control processing of the altitude to maintain a constant altitude difference with the manned aircraft 30, the manned aircraft 30 Manned-unmanned aerial vehicle collision prevention communication system, characterized in that to avoid the risk of collision with.
The method of claim 1,
The UAV flight information database of the unmanned aerial vehicle 10 includes unique UAV identification information of the unmanned aerial vehicle 10;
The communication database of the manned aircraft 30 includes UAV information data including a plurality of UAV 10 unique UAV identification information;
The communication control module of the manned aircraft 30 transmits the manned aircraft information to the unmanned aerial vehicle 10 included in the UAV information data only through the transponder's responder using the UAV identification information unique to the unmanned aerial vehicle 10. Manned-unmanned aircraft collision prevention communication system.
A UAV-SSR Sytem composed of a UAV transponder composed of a question receiver and a responder, and a UAV interrogator composed of a transmitter, a receiver, and a decoder; A UAV communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with a GCS communication transmitter-receiver of the GCS; UAV communication control module; An unmanned aerial vehicle 10 having a communication system including a UAV flight information database;
A GCS communication transmitter-receiver configured of a main communication transmitter-receiver and a preliminary communication transmitter-receiver capable of interworking with the UAV communication transmitter-receiver of the unmanned aerial vehicle 10; A GCS communication control module; A GCS flight information database; A GCS 20 having a communication system comprising a pilot manipulator;
When the unmanned aerial vehicle 10 and the GCS 20 having the above configuration are operated in plural flights, the communication system of the unmanned aerial vehicle 10 and the other unmanned aerial vehicle 10 'may be interoperable with each other to exchange predetermined information. Unmanned-unmanned aircraft collision prevention communication system.
The method of claim 5,
The UAV flight information database further includes anti-collision automatic control processing data,
The UAV communication control module of the unmanned aerial vehicle 10 predicts the altitude and speed of another unmanned aerial vehicle 10 'by using the unmanned aerial vehicle information of another unmanned aerial vehicle 10' obtained through the UAV interrogator. And the UAV communication control module automatically controls the speed of the unmanned aerial vehicle 10 itself by using the generated prediction information, and automatically controls the altitude so as to maintain a constant altitude difference with the other unmanned aerial vehicle 10 '. Unmanned-unmanned aircraft collision prevention communication system, characterized in that any one or more of the automatic control process to avoid the risk of collision with another unmanned aerial vehicle (10 ').
The method of claim 5,
The UAV flight information database of the unmanned aerial vehicle 10 includes unique UAV identification information of the unmanned aerial vehicle 10;
The UAV communication database 'of the other unmanned aerial vehicle 10' includes UAV information data containing a plurality of UAV unique UAV identification information;
The communication control module of the other unmanned aerial vehicle 10 'uses another UAV through the transponder responder only to the unmanned aerial vehicle 10 included in the UAV information data using the unique UAV identification information of the unmanned aerial vehicle 10. And an unmanned aerial vehicle information of (10 ').

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