KR102220388B1 - Induction deception device and method for controlling the movement of induced deception using rcs pattern - Google Patents

Abstract

The present invention relates to an induction deception device and a method for controlling the movement of an induction deception body using radar cross section (RCS) patterns. According to the present invention, the induction deception device for controlling the movement of the induction deception body using RCS patterns comprises: an RCS pattern acquisition unit which collects and acquires the RCS pattern information of a system and the CRS pattern information of the induction deception body; an RCS pattern synthesizing unit which synthesizes the RCS pattern information of the system and the RCS pattern information of the induction deception body, which are acquired; a first synthesized RCS pattern maximization unit which maximizes the RCS pattern information of the system and the RCS pattern information of the induction deception body, which are synthesized; a deception body rotation lock status determination unit which, when the RCS pattern information of the system and the RCS pattern information of the induction deception body, which are synthesized, are maximized, determines whether the induction deception body is rotationally locked or not; and a deception body movement control unit which, when the induction deception body is rotationally locked, controls the movement of the induction deception body. The present invention is able to improve system′s ability to avoid an attack from an induction aircraft.

Description

An induced deception device that controls the movement of an induced deceiving body using an RCS pattern, and its method {INDUCTION DECEPTION DEVICE AND METHOD FOR CONTROLLING THE MOVEMENT OF INDUCED DECEPTION USING RCS PATTERN}

The present invention relates to a guided deceptive device and method for controlling the movement of a guided deceptive body using an RCS pattern, and in more detail, the radar cross section (RCS) pattern information of the system and radar reflection of the guided deceptive body The present invention relates to a guided deception apparatus and a method for controlling the movement of a guided deceptive object by using an RCS pattern to protect against an attack of a guided vehicle by synthesizing area pattern information.

Conventionally, a general noise jamming signal is mainly emitted for only an induction machine of an unmanned aerial vehicle, thereby disabling a GNSS (global navigation satellite system) receiver of an unmanned aerial vehicle.

However, the conventional unmanned aerial vehicle induction deception method mainly requires accurate location information of the unmanned aerial vehicle, and has a problem in that a jamming signal should be transmitted in real time using the location information. In other words, only 1:1 response to the target is possible.

In this case, the unmanned aerial vehicle cannot accurately know the current location information, causing a flight disruption. However, since the direction information can still be recognized, it is possible to navigate the drone to the enemy's territory and retrieve it by the enemy.

However, such a general jamming signal only disturbs the operation of the UAV, and there is a problem in that it is not easy to crash the UAV or lure it to a friendly territory and capture it.

In this regard, Korean Patent Application Publication No. 2017-0057966 discloses "an apparatus and method for generating a radar tracking-based satellite navigation deception signal".

The present invention is invented to solve the above problems, and controls the movement of the guided deceiver using an RCS pattern that synthesizes and maximizes the radar reflection area pattern information of the system and the radar reflection area pattern information of the guided deceiver. An object thereof is to provide a guided deception device and a method thereof.

In addition, the present invention uses the RCS pattern to control the movement of the guided deceiver by determining whether the rotation of the guided deceiver is locked when the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized. It is an object of the present invention to provide a guided deception device and a method for controlling the movement of a guided deceptive body.

In order to achieve the above object, the guided deception device for controlling the movement of the guided deceptive body using the RCS pattern according to the present invention includes information on the radar cross section (RCS) pattern of the system and the radar reflection area of the guided deceptive body. An RCS pattern acquisition unit that collects and acquires pattern information; An RCS pattern synthesizing unit for synthesizing the radar reflection area pattern information of the obtained system and the radar reflection area pattern information of the guided deceiver; A first synthetic RCS pattern maximizing unit for maximizing radar reflection area pattern information of the synthesized system and radar reflection area pattern information of the guided deceiver; When the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, the deceiver rotation lock determination unit determines whether or not the guided deceiver is locked; And a deceptive body movement control unit that controls the movement of the deceptive body when the rotation of the deceptive body is locked.

In addition, the RCS pattern acquisition unit may include a system RCS information collection unit that collects radar reflection area pattern information on a three-dimensional space of the system; And a deceptive object RCS information collection unit that collects radar reflection area pattern information for a three-dimensional space of the guided deceptive object.

In addition, the RCS pattern synthesis unit synthesizes the radar reflection area pattern information of the collected system and the radar reflection area pattern information of the guided deceiver by reflecting the rotation angle of the guided deceiver calculated based on the orientation angle of the guided deceiver derived later. Characterized in that.

In addition, the first synthesized RCS pattern maximizing unit rotates the guided deceptive body in the direction of the guided vehicle to maximize the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body.

In addition, the deceptive body rotation lock determination unit maximizes the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body, and intercepts the target of the system tracked by the guided vehicle to the guided deceptive body. It is characterized in that it is determined whether the rotation of the is locked.

In addition, it characterized in that it comprises a first deceptive body rotation angle calculation unit for calculating the rotation angle of the movement-controlled guided deceptive body using the collected guided vehicle detection information.

In addition, it is characterized by including a second synthetic RCS pattern maximizing unit for maximizing radar reflection area pattern information of the system synthesized based on the calculated rotation angle of the guided deceiver and the radar reflection area pattern information of the guided deceiver.

In addition, when the rotation of the guided deceiver is not locked, it is synthesized based on the location of the guided deceiver based on the collected guided vehicle detection information, system navigation information, and relative position information calculated based on the guided deceiver navigation information. It characterized by including a deceptive body orientation angle derivation unit for deriving a directing angle of the guided deceptive body for maximizing the radar reflection area pattern information of the system and the radar reflection area pattern information of the guided deceiver.

In addition, it characterized in that it comprises a second deceptive body rotation angle calculation unit for calculating the rotation angle of the guided deceptive body in which the derived orientation angle of the deceptive body is reflected.

In addition, the vehicle detection information collection unit for collecting the guided vehicle detection information; A system navigation information collection unit that collects system navigation information; A deceiver navigation information collection unit that collects navigation information of a guided deceiver; And a relative position information calculation unit that calculates relative position information based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information.

In order to achieve the above object, the guided deception method for controlling the movement of the guided deceptive body using the RCS pattern according to the present invention includes, by an RCS pattern acquisition unit, radar cross section (RCS) pattern information and Collecting and obtaining radar reflection area pattern information of the guided deceiver; Synthesizing, by the RCS pattern synthesis unit, radar reflection area pattern information of the obtained system and radar reflection area pattern information of the guided deceiver; Maximizing the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver, by a first synthesis RCS pattern maximizing unit; Determining whether or not rotation of the guided deceiver is locked when the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized by the deceiver rotation locking unit; And controlling the movement of the induced deceptive body when the rotation of the deceptive body is locked by the deceptive body movement control unit.

In addition, when the rotation of the guided deceptive body is locked, after the step of controlling the movement of the guided deceptive body, the step of calculating the rotation angle of the movement-controlled guided deceptive body using the collected guided vehicle detection information It is characterized.

In addition, after calculating the rotation angle of the guided deceptive body that has been controlled using the collected guided vehicle detection information, the radar reflection area pattern information of the synthesized system based on the calculated rotation angle of the guided deceptive body and the It characterized in that it comprises the step of maximizing the radar reflection area pattern information.

In addition, when the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, after the step of determining whether the guided deceiver is locked or not, the step of collecting guided vehicle detection information ; Collecting system navigation information; Collecting navigation information for guided deceivers; Calculating relative position information based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information; And based on the calculated relative position information, the radar reflection area pattern information of the system synthesized based on the position of the guided deceiver and the radar reflection area pattern information of the guided deceiver is derived. It characterized in that it comprises a step.

In addition, based on the calculated relative position information, we derive the orientation angle of the guided deceiver to maximize the radar reflection area pattern information of the system synthesized based on the location of the guided deceiver and the radar reflection area pattern information of the guided deceiver. After the step of, it characterized in that it comprises the step of calculating the rotation angle of the guided deceptive body reflecting the orientation angle of the derived deceptive body.

In addition, after the step of calculating the rotation angle of the guided deceptive body that reflects the orientation angle of the derived guided deceptive body, the system was collected by reflecting the rotation angle of the guided deceptive body calculated based on the derived orientation angle. It is characterized in that the radar reflection area pattern information and the radar reflection area pattern information of the guided deceiver are synthesized.

In order to achieve the above object, a guided deceptive device for controlling the movement of a guided deceptive body using the RCS pattern according to the present invention and its method synthesizes the radar reflection area pattern information of the system and the radar reflection area pattern information of the guided deceptive body. And, if the rotation of the guided deceptive is locked after maximizing the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body, the target of the system being tracked by the guided vehicle is moved to the guided deceptive. By grasping it, there is an effect of improving the ability to evade the system from the attack of the guided vehicle.

In addition, the present invention has the effect of inducing the direction of the target of the guided vehicle to move toward the guided deceptive continuously by maintaining the maximum radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body. .

1 is a diagram for explaining the concept of a guided deception system according to the present invention.
2 is a view for explaining the configuration of a guided deception device for controlling the movement of a guided deceptive body using an RCS pattern according to the present invention.
3 is a view for explaining the sequence of a guided deception method for controlling movement of a guided deceptive body using an RCS pattern according to the present invention.

In the present invention, various modifications may be made and various embodiments may be provided, and specific embodiments will be illustrated in the drawings and described in detail.

However, this is not intended to limit the present invention to a specific embodiment, it is to be understood to include all changes, equivalents, or substitutes included in the spirit and scope of the present invention. In describing each drawing, similar reference numerals have been used for similar elements.

When a component is referred to as being "connected" or "connected" to another component, it is understood that it may be directly connected or connected to the other component, but other components may exist in the middle. Should be. On the other hand, when a component is referred to as being "directly connected" or "directly connected" to another component, it should be understood that there is no other component in the middle.

The terms used in the present application are only used to describe specific embodiments, and are not intended to limit the present invention. Singular expressions include plural expressions unless the context clearly indicates otherwise. In the present application, terms such as "comprise" or "have" are intended to designate the presence of features, numbers, steps, actions, components, parts, or combinations thereof described in the specification, but one or more other features. It is to be understood that the presence or addition of elements or numbers, steps, actions, components, parts, or combinations thereof, does not preclude in advance.

Hereinafter, preferred embodiments of the present invention will be described in more detail with reference to the accompanying drawings. Hereinafter, the same reference numerals are used for the same elements in the drawings, and duplicate descriptions for the same elements are omitted.

1 is a diagram for explaining the concept of a guided deception system according to the present invention.

Referring to FIG. 1, a guided vehicle equipped with an RF searcher is approaching the system based on a searcher. At this time, the system also moves while monitoring and reconnaissance, so check the approach of the guided vehicle and acquire location and direction information. If it is determined that it is a dangerous situation based on the acquired location and defense information, the guided deceptive is floated and moved to a place a certain distance from the system.

Here, the structure of the guided deceptive body was made to form a pattern in a specific direction in consideration of the frequency and reflection characteristics of RF, and the guided deceptive body according to the present invention has a flying wing such as a thruster or a drone and guided into a specific direction. It is assumed that it is a hovering type that moves by installing the structure of.

Based on the above configuration, the present invention synthesizes the radar reflection area (RCS) pattern information of the system and the radar reflection area pattern information of the guided deceptive body, and the radar reflection area pattern information and guided deception of the synthesized system. We intend to propose a signal processing and deception control technology to guide the target of the guided vehicle to the guided deceptive by maintaining the radar reflection area pattern information of the body to be maximized.

2 is a view for explaining the configuration of a guided deception device for controlling the movement of a guided deceptive body using an RCS pattern according to the present invention.

Referring to FIG. 2, the guided deception device 100 for controlling the movement of the guided deceptive body using the RCS pattern according to the present invention includes an RCS pattern acquisition unit 110, an aircraft detection information collection unit 113, System navigation information collection unit 114, deceptive navigation information collection unit 115, RCS pattern synthesis unit 120, first synthesis RCS pattern maximization unit 130, deceiver rotation lock determination unit 140, deception The body movement control unit 150, the first deceptive body rotation angle calculation unit 151, the second synthetic RCS pattern maximization unit 160, the deceptive body orientation angle derivation unit 170, the second deception body rotation angle calculation unit 180 ) And a relative location information calculation unit 190.

The RCS pattern acquisition unit 110 collects and acquires radar reflection area (RCS) pattern information of the system and radar reflection area pattern information of the guided deceiver.

To this end, the RCS pattern acquisition unit 110 includes a system RCS information collection unit 111 and a deceptive RCS information collection unit 112.

The system RCS information collection unit 111 collects radar reflection area pattern information for a three-dimensional space of the system.

The deceptive RCS information collection unit 112 collects radar reflection area pattern information for the three-dimensional space of the guided deceptive.

The vehicle detection information collection unit 113 collects guided vehicle detection information including at least one of azimuth, elevation, distance, and speed of the guided vehicle.

The system navigation information collection unit 114 collects system navigation information including at least one of latitude, longitude, and altitude of the system.

The deceptive navigation information collection unit 115 collects guided deceptive navigation information including at least one of latitude, longitude, altitude, and posture of the guided deceptive.

The RCS pattern synthesis unit 120 synthesizes the radar reflection area pattern information of the obtained system and the radar reflection area pattern information of the guided deceiver.

In addition, the RCS pattern synthesis unit 120 reflects the rotation angle of the guided deceptive body calculated based on the orientation angle of the guided deceptive body, which is then derived, and reflects the radar reflection area pattern information of the system and the radar reflection area pattern information of the guided deceptive body. Can be synthesized.

The first synthetic RCS pattern maximizing unit 130 maximizes radar reflection area pattern information of the synthesized system and radar reflection area pattern information of the guided deceptive body.

The first synthesis RCS pattern maximizing unit 130 rotates the guided deceptive body in the direction of the guided vehicle so that the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body are maximized.

When the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, the deceiver rotation lock determination unit 140 determines whether the guided deceiver is locked.

That is, the deceptive body rotation lock determination unit 140 maximizes the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body, and intercepts the target of the system tracked by the guided vehicle to the guided deceptive body. It can be determined whether the rotation of the guiding deceptive is locked. This is because the basic principle of detection and tracking of the RF searcher detected in the guided vehicle is to identify the target in the direction of maximizing the RCS.

The deceiver movement control unit 150 controls the movement of the guided deceiver when the rotation of the guided deceiver is locked.

That is, the deceptive body movement control unit 150 intercepts the target of the system being tracked by the guided vehicle as a guided deceptive body, and then moves the guided deceptive body to decrease the distance from the system. This is to minimize the damage to the system due to the explosion after the collision between the guided deceptive and the guided vehicle by moving the position of the target.

The first deceptive body rotation angle calculation unit 151 calculates the rotation angle of the movement-controlled guided deceptive body using the collected guided vehicle detection information.

The second synthesized RCS pattern maximizing unit 160 maximizes radar reflection area pattern information of the synthesized system based on the calculated rotation angle of the guided deceiver and radar reflection area pattern information of the guided deceiver.

That is, the second synthetic RCS pattern maximizing unit 160 is to continuously recalculate the position on the geometric structure and maximize the laser reflection area based on this because the relative position changes when the guiding deceptive body moves.

The relative position information calculation unit 190 calculates relative position information based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information.

The deceptive body orientation angle derivation unit 170 is based on the calculated relative position information when the rotation of the guided deceiver is not locked, the radar reflection area pattern information and guided deception of the system synthesized based on the location of the guided deceiver. The orientation angle of the guided deceptive body is derived to maximize the radar reflection area pattern information of the body.

The second deceiving body rotation angle calculation unit 180 calculates the rotation angle of the guided deceiver in which the orientation angle of the derived guided deceiver is reflected, and reflects this to the RCS pattern synthesis unit 120 described above to reflect the radar reflection area of the system. The structure of the guided deceiver is continuously rotated by synthesizing the pattern information and the radar reflection area pattern information of the guided deceiver.

3 is a diagram for explaining a sequence of a guided deception method for controlling movement of a guided deceptive body using an RCS pattern according to the present invention.

3 is a guided deception method for controlling the movement of a guided deceptive body using an RCS pattern according to the present invention, which uses a guided deception device that controls the movement of the guided deceptive body using the RCS pattern described above, and the following description is repeated. Is omitted.

First, the radar reflection area (RCS: Radar Cross Section) pattern information of the system and the radar reflection area pattern information of the guided deceiver are collected and acquired (S100).

Step S100 collects radar reflection area pattern information for the 3D space of the system and radar reflection area pattern information for the 3D space of the guided deceiver.

And, guided vehicle detection information including at least one of azimuth, elevation, distance and speed of the guided vehicle, system navigation information including at least one of the system's latitude, longitude and altitude, and the latitude, longitude of the guided deceptive, Induction deceptive navigation information including at least one of altitude and posture is collected (S101).

Next, relative position information is calculated based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information (S103).

After the step S100, the radar reflection area pattern information of the obtained system and the radar reflection area pattern information of the guided deceiver are synthesized (S110).

Next, the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized (S120).

Step S120 rotates the guided vehicle in the direction of the guided vehicle so that the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided vehicle are maximized.

Next, when the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body are maximized, it is determined whether or not the guided deceptive body is locked (S130).

In step S130, the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, and the target of the system being tracked by the guided vehicle is intercepted as a guided deceiver to determine whether the rotation of the guided deceiver is locked. I can judge. This is because the basic principle of detection and tracking of the RF searcher detected in the guided vehicle is to identify the target in the direction of maximizing the RCS.

In step S130, when it is determined that the rotation of the induced deceptive body is locked, the movement of the induced deceptive body is controlled (S140).

In step S140, the target of the system being tracked by the guided vehicle is intercepted as a guided deceiver, and then the guided deceiver is moved to reduce the distance from the system. This is to minimize the damage to the system due to the explosion after the collision between the guided deceptive and the guided vehicle by moving the position of the target.

Next, the rotation angle of the movement-controlled guided deceptive body is calculated using the guided vehicle detection information collected in step S101 (S150).

Next, the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized based on the calculated rotation angle of the guided deceiver (S160).

Step S160 is to maximize the laser reflection area based on the continuous recalculation of the geometrical position because the relative position changes when the guided deceptive body moves.

On the other hand, if it is determined that the rotation of the guided deceiver is not locked in step S130, based on the relative position information calculated in step S103, the radar reflection area pattern information and guidance of the system synthesized based on the location of the guided deceiver The orientation angle of the guided deceptive body is derived for maximizing the radar reflection area pattern information of the deceptive body (S170).

Next, the rotation angle of the induced deceptive body is calculated in which the orientation angle of the derived deceptive body is reflected (S180).

In step S180, to step S110 of synthesizing the radar reflection area pattern information of the system and the radar reflection area pattern information of the collected system by reflecting the rotation angle of the guided deceiver calculated based on the orientation angle of the derived guided deceiver. Move and continuously rotate the structure of the guiding deceptive.

The functional operations described in this specification and embodiments related to the subject are implemented in digital electronic circuits, computer software, firmware, or hardware, including structures disclosed in this specification and structural equivalents thereof, or in a combination of one or more of them. It is possible.

Embodiments of the subject matter described herein include one or more of a computer program product, i.e., one or more of computer program instructions encoded on a tangible program medium for execution by or to control its operation by a data processing device. It can be implemented as a module. The tangible program medium may be a radio wave signal or a computer-readable medium. A radio wave signal is an artificially generated signal, such as a machine-generated electrical, optical or electromagnetic signal, generated to encode information for transmission to a suitable receiver device for execution by a computer. The computer-readable medium may be a machine-readable storage device, a machine-readable storage substrate, a memory device, a combination of materials that affect a machine-readable radio wave signal, or a combination of one or more of them.

Computer programs (also known as programs, software, software applications, scripts, or code) can be written in any form of a compiled or interpreted language or a programming language, including a priori or procedural language, and can be written as a standalone program or module, It can be deployed in any form, including components, subroutines, or other units suitable for use in a computer environment.

Computer programs do not necessarily correspond to files on the file device. A program may be in a single file provided to the requested program, or in multiple interactive files (e.g., files in which one or more stores a module, subprogram, or part of code), or in a file that holds other programs or data. Some (eg, one or more stored within a markup language document may be stored within a script).

The computer program may be deployed to run on one computer or multiple computers located at one site or distributed across a plurality of sites and interconnected by a communication network.

Additionally, the logical flows and structural block diagrams described in this patent document describe the corresponding actions and/or specific methods supported by the corresponding functions and steps supported by the disclosed structural means. It can also be used to build software structures and algorithms and their equivalents.

The processes and logic flows described herein may be executed by a programmable processor, one or more executing a computer program in order to perform a function by operating on received data and generating an output.

Processors suitable for execution of computer programs include, for example, both general purpose and special purpose microprocessors and any one or more of any type of digital computer being a processor. Typically, the processor will receive instructions and data from read-only memory, random access memory, or both.

The key elements of a computer are one or more memory devices for storing instructions and data, and a processor for performing the instructions. In addition, computers are generally operable to receive data from, transfer data to, or perform both of the mass storage devices, such as one or more for storing data, such as magnetic, magneto-optical disks or optical disks. Combined or will include. However, the computer does not need to have such a device.

The present description presents the best mode of the invention, and provides examples to illustrate the invention and to enable those skilled in the art to make and use the invention. The thus written specification does not limit the present invention to the specific terms presented.

Accordingly, although the present invention has been described in detail with reference to the above-described examples, those skilled in the art can make modifications, changes, and modifications to these examples without departing from the scope of the present invention. In short, in order to achieve the intended effect of the present invention, it is not necessary to separately include all functional blocks shown in the drawings or to follow all the sequences shown in the drawings as shown in the order shown. Note that it may fall within the range.

100:
110: RCS pattern acquisition unit;
120: RCS pattern synthesis unit
130: first synthesis RCS pattern maximization unit
140: Deception body rotation lock determination unit
150: deceiver movement control unit
160: second synthesis RCS pattern maximizer
170: deceptive body orientation angle derivation unit
180: second deceiver rotation angle calculation unit
190: relative position information calculation unit

Claims (16)

An RCS pattern acquisition unit that collects and acquires radar reflection area (RCS) pattern information of the system and radar reflection area pattern information of a guided deceiver;
An RCS pattern synthesizing unit for synthesizing the radar reflection area pattern information of the obtained system and the radar reflection area pattern information of the guided deceiver;
A first synthetic RCS pattern maximizing unit for maximizing radar reflection area pattern information of the synthesized system and radar reflection area pattern information of the guided deceiver;
When the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, the deceiver rotation lock determination unit determines whether or not the guided deceiver is locked; And
A deceptive body movement control unit for controlling the movement of the deceptive body when the rotation of the deceptive body is locked;
Guided deception device for controlling the movement of the guided deceptive body using the RCS pattern comprising a. The method of claim 1,
The RCS pattern acquisition unit,
A system RCS information collection unit that collects radar reflection area pattern information on a three-dimensional space of the system; And
A deceiver RCS information collection unit that collects radar reflection area pattern information for a three-dimensional space of the guided deceiver;
Guided deception device for controlling the movement of the guided deceptive body using the RCS pattern comprising a. The method of claim 1,
The RCS pattern synthesis unit synthesizes the radar reflection area pattern information of the collected system by reflecting the rotation angle of the guided deceiver calculated based on the orientation angle of the guided deceiver and the radar reflection area pattern information of the guided deceiver. A guided deception device that controls the movement of a guided deceptive body using the RCS pattern, characterized by. The method of claim 1,
The first synthetic RCS pattern maximizer rotates the guided deceptive body in the direction of the guided vehicle to maximize the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body. A guided deception device that controls the movement of a guided deceptive body. The method of claim 1,
The deceptive body rotation lock determination unit maximizes the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceptive body, and intercepts the target of the system being tracked by the guided vehicle to the guided deceptive body. A guided deception device for controlling the movement of a guided deceptive body using an RCS pattern, characterized in that it determines whether or not is locked. The method of claim 1,
A guided deception that controls the movement of the guided deceptive body using an RCS pattern, characterized in that it includes a first deceptive body rotation angle calculation unit that calculates the rotation angle of the guided deceptive body that has been controlled using the collected guided vehicle detection information. Device. The method of claim 6,
Using the RCS pattern, characterized in that it includes a second synthetic RCS pattern maximizing unit that maximizes radar reflection area pattern information of the system synthesized based on the calculated rotation angle of the guided deceiver and the radar reflection area pattern information of the guided deceiver. A guided deception device that controls the movement of a guided deceptive body. The method of claim 1,
When the rotation of the guided deceiver is not locked, based on the collected guided vehicle detection information, system navigation information, and relative position information calculated based on the guided deceiver navigation information, the synthesized system based on the location of the guided deceiver Movement of the guided deceptive body using the RCS pattern, characterized in that it includes a deceptive body oriented angle derivation unit that derives the orientation angle of the guided deceptive to maximize radar reflection area pattern information and the radar reflection area pattern information of the guided deceptive. Induction deception device to control. The method of claim 8,
A guided deception device for controlling the movement of the guided deceptive body using an RCS pattern, comprising: a second deceptive body rotation angle calculation unit that calculates a rotation angle of the guided deceptive body in which the derived orientation angle of the guided deceptive body is reflected. The method of claim 1,
A vehicle detection information collection unit for collecting guided vehicle detection information;
A system navigation information collection unit that collects system navigation information;
A deceiver navigation information collection unit that collects navigation information of a guided deceiver; And
A relative position information calculation unit that calculates relative position information based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information;
Guided deception device for controlling the movement of the guided deceptive body using the RCS pattern comprising a. Collecting and obtaining, by the RCS pattern acquisition unit, radar cross section (RCS) pattern information of the system and radar reflection area pattern information of the guided deceiver;
Synthesizing, by the RCS pattern synthesis unit, radar reflection area pattern information of the obtained system and radar reflection area pattern information of the guided deceiver;
Maximizing the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver, by a first synthesis RCS pattern maximizing unit;
Determining whether or not rotation of the guided deceiver is locked when the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized by the deceiver rotation locking unit; And
Controlling the movement of the guided deceiver when the rotation of the guided deceiver is locked by the deceiving body movement control unit;
Induction deception method for controlling the movement of the induced deceptive body using the RCS pattern, characterized in that it comprises a. The method of claim 11,
When the rotation of the induced deceiver is locked, after the step of controlling the movement of the induced deceiver,
A guided deception method for controlling the movement of the guided deceptive body using an RCS pattern, comprising the step of calculating a rotation angle of the guided deceptive body that has been controlled by using the collected guided vehicle detection information. The method of claim 12,
After calculating the rotation angle of the movement-controlled guided deceptive body using the collected guided vehicle detection information,
Movement of the guided deceiver using an RCS pattern, characterized in that it includes maximizing the radar reflection area pattern information of the synthesized system based on the calculated rotation angle of the guided deceiver and the radar reflection area pattern information of the guided deceiver. Induction deception method to control, The method of claim 11,
When the radar reflection area pattern information of the synthesized system and the radar reflection area pattern information of the guided deceiver are maximized, after the step of determining whether the guided deceiver is locked or not,
Collecting guided vehicle detection information;
Collecting system navigation information;
Collecting navigation information for guided deceivers;
Calculating relative position information based on the collected guided vehicle detection information, system navigation information, and guided deceptive navigation information; And
Based on the calculated relative position information, the step of deriving the orientation angle of the guided deceiver to maximize the radar reflection area pattern information of the system synthesized based on the position of the guided deceiver and the radar reflection area pattern information of the guided deceiver. Induction deception method for controlling the movement of the induced deceptive body using the RCS pattern, characterized in that it comprises a. The method of claim 14,
Based on the calculated relative position information, the step of deriving the orientation angle of the guided deceiver to maximize the radar reflection area pattern information of the system synthesized based on the position of the guided deceiver and the radar reflection area pattern information of the guided deceiver. Since the,
A guided deception method for controlling the movement of the guided deceiver using an RCS pattern, comprising the step of calculating a rotation angle of the guided deceiver in which the derived orientation angle of the guided deceiver is reflected. The method of claim 14,
After the step of calculating the rotation angle of the induced deceiver in which the orientation angle of the derived guided deceiver is reflected,
An RCS pattern characterized by synthesizing the radar reflection area pattern information of the system and the radar reflection area pattern information of the collected system by reflecting the rotation angle of the guided deceiver calculated based on the derived orientation angle of the guided deceiver. A guided deception method that controls the movement of a guided deceptive body using.

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