KR20200127477A - Apparatus and method for simulating avionics coupling of radar - Google Patents

Abstract

The present invention relates to an avionics-linked simulation apparatus for a radar to verify a design and an avionics-linked operation of a radar system, and a method thereof. According to the present invention, the avionics-linked simulation apparatus for a radar comprises: an avionics-linked simulation unit linking the state and operation information of each component of a radar at a radar system level in accordance with a control compound corresponding to a user interface and generating scenario data and a radar operation command for simulating avionics equipment; a radar system operation simulation unit checking operation of each component of the radar and simulating an operation state and an operation of the radar in accordance with a control command received from the avionics-linked simulation unit to transfer a simulation result to the avionics-linked simulation unit; and a radar simulation execution unit executing simulation for antenna effect, detection performance, tracking performance, and beam scheduling of the radar in accordance with the operation state of the radar received from the avionics-linked simulation unit.

Description

A radar navigation interlocking simulation device and its method {APPARATUS AND METHOD FOR SIMULATING AVIONICS COUPLING OF RADAR}

The present invention relates to the operation of a radar mounted on an aircraft (aircraft) and a navigation linkage simulation technique, and more particularly, a radar system through a radar function and performance analysis by establishing a flight warfare linkage simulation environment between an aircraft (aircraft) and a radar The present invention relates to an apparatus and method for simulating a radar flight linkage capable of verifying the design and operation of flight linkage.

As is known, the use of M&S (Modeling and Simulation, modeling and simulation) in the fields of required analysis, development, and test evaluation of weapon systems in defense-related technologies is a very important factor in terms of reducing development costs and lowering development risks. There is a situation.

The process of developing and verifying the radar system of an aircraft (aircraft) in such defense-related element technologies is not only a radar simulation environment, but also a flight-related simulation environment between aircraft and radar, in consideration of the technical difficulty of development and enormous budget investment. In addition, it is essential to verify the contents of the radar system design through the analysis of the function and performance of the radar, and to verify the operational logic when interlocking with the aircraft.

In particular, one of the important factors to consider in the development of an aircraft radar system is that the radar is the aircraft's avionics equipment, such as MC (Mission Computer), EGI (Embedded GPS-INS), EWS (Electronic Warfare System), and other aircraft subsystems and missiles. It should be linked with aircraft components in real time.

However, in the process of developing a radar system, the conventional radar simulation system corresponds to an engineering-grade radar M&S at the sub-system level, and focuses only on verifying the function or performance of the radar by business unit, without considering the above interlocking. There is a problem that there is a problem, and due to this fundamental problem, there is a limit in effectively verifying the system operability according to the aircraft system mission performance procedure.

Korean Patent Publication No. 2018-0119931 (Publication date: 2018. 11. 05.)

An object of the present invention is to provide a radar navigation-related simulation apparatus and method capable of executing a system-level and engagement-class aircraft radar simulation, including a navigation linkage, by extending an existing sub-system-level engineering-grade radar simulation system.

The present invention is a radar navigation link simulation device capable of effectively verifying the design of a radar system and operation of a flight linkage through the function and performance analysis of the radar by establishing a simulation environment for navigation linkage between an aircraft (aircraft) and a radar, and I want to provide you with that.

An object of the present invention is to provide a computer-readable recording medium in which a computer program is stored that allows a processor to perform a simulation method of radar flight interlocking that can effectively verify the design of a radar system and operation of flight interlocking.

The problem to be solved by the present invention is not limited to the ones mentioned above, and another problem to be solved that is not mentioned can be clearly understood by those of ordinary skill in the art from the following descriptions. will be.

According to an aspect of the present invention, in accordance with a control command corresponding to a user interface, the state and operation information of each component of the radar are linked at the level of the radar system, and scenario data and radar operation command for simulation of avionics equipment Operation of a radar system that simulates the operation of each component of the radar, and simulates the operation state and operation mode of the radar according to a control command from the navigation linkage simulation unit and the aircraft flight linkage simulation unit to generate a Flight interlocking simulation of a radar including a simulation unit and a radar simulation execution unit that simulates the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the operating state of the radar received from the flight combat linkage simulation unit Device can be provided.

The radar system operation simulation unit includes simulation information for generating frequency signal waveform information suitable for each operation mode of the radar and an information transmission/reception simulation unit for generating its own state information, and beam emission for a transmission signal and reception from a simulated target. An antenna simulation unit that generates antenna configuration information and its own state information to apply the effect of the antenna to the signal, and simulation information, antenna configuration information, and each component provided from the information transmission/reception simulation unit and the antenna simulation unit. Based on the state information, it may include a radar signal processing simulation unit that performs the operation check of each component of the radar, the operation state control and simulation for the operation mode.

The radar signal processing simulation unit of the present invention may selectively simulate air-to-air, air-to-ground, and air-to-sea modes, respectively.

The radar system operation simulation unit of the present invention simulates power supply to the information transmission/reception simulation unit, the antenna simulation unit, and the radar signal processing simulation unit based on a power control command, and the radar signal processing simulation of its own state information. It may further include a power supply simulation unit for transmitting to the unit.

The radar simulation execution unit of the present invention includes a control control simulation unit for scheduling operation and implementation of an operation mode of the radar, data processing for detection and tracking of the radar, and a setting of a radar beam, and from the control control simulation unit. An antenna simulation unit that models the antenna effect on the gain and phase of the transmitted and received signals by applying an antenna beam pattern according to the antenna steering direction requested by the user, and the self-speed compensation and pulse for the signal received through the antenna simulation unit It may include a signal processing simulation unit that performs compression and Doppler processing and generates a range-doppler map through Fast Fourier Transform (FFT).

The control control simulation unit of the present invention includes a detailed mode management model unit in charge of operation and implementation of an operation mode for a radar operation mode commanded from the radar system operation simulation unit, and a search range, search pattern, and search cycle of each mode. , Controls a radar search setting value including the next search position, and performs data processing for radar detection and tracking including target association, target tracking, and inter-beam processing using target data received from the signal processing simulation unit. A search and tracking management model unit, and a beam steering management model unit that sets radar beam information to radiate a beam to a steering position determined by the search and tracking management model unit, and performs periodic scheduling on the set information. Can include.

When the air-to-air search and tracking mode is set according to the user interface, the detailed mode management model unit of the present invention can determine whether a corresponding mode can be executed, change a radar setting value according to mode change, and change a beam steering method. have.

The signal processing simulation unit of the present invention includes an FFT performance model unit that generates the range Doppler map for estimating a target state by performing the FFT on the received signal, and a constant CFAR (CFAR) using the generated range Doppler map. False Alarm Rate) a CFAR execution model unit that extracts target information through a detector, an angle calculation model unit that calculates an angle to the target through the value extracted through the CFAR execution model unit, and the calculated angle of the target. It may include an ambiguity removal model unit that derives the position and speed of the target through ambiguity removal.

According to another aspect, the present invention includes the steps of generating scenario data and radar operation commands for simulating flight movement of a radar based on a control command generated according to a user interface, and each of the radars according to the generated control command. Checking the operation of components, simulating the operation state and operation mode of the radar, and the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the operation state of the radar received through the simulating step. It is possible to provide a simulation method for interlocking flight of a radar including the step of executing the simulation.

According to another aspect, the present invention is a computer-readable recording medium in which a computer program for causing a processor to perform a radar flight motion-linked simulation method is stored, wherein the motion-linked simulation method is based on a control command generated according to a user interface. Generating scenario data and a radar operation command for simulating the navigation linkage of the radar, checking the operation of each component of the radar according to the generated control command, and simulating the operation state and operation mode of the radar, It is possible to provide a computer-readable recording medium comprising the step of executing simulations for the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the radar operation state received through the simulating step.

According to an embodiment of the present invention, it is possible not only to perform an analysis of aircraft radar performance and to effectively verify the functional requirements, but also by comprehensively verifying the operation state and operation procedure of the radar according to the mission performance procedure of the aircraft radar. Anomalies, errors and omissions in the system design can be effectively verified, and through this, the system operability of aircraft radar can be effectively verified.

In addition, according to an embodiment of the present invention, by establishing a simulation environment for navigation linkage between the aircraft and the radar, it is possible to verify the design of the radar system and the operation of the navigation linkage through the function and performance analysis of the radar, thereby developing the aircraft radar system. Not only can the cost be drastically reduced, but the risk of development delays and failures can be significantly reduced.

1 is an M&S hierarchy diagram of an aircraft radar system.
2 is a conceptual diagram corresponding to a simulation apparatus according to an embodiment of the present invention to an aircraft system M&S hierarchy diagram.
3 is a block diagram of an apparatus for simulating a radar navigation system according to an embodiment of the present invention.
4 is a detailed block diagram of a radar system operation simulation unit shown in FIG. 3.
5 is a detailed block diagram of a radar simulation execution unit shown in FIG. 3.
6 is a flow chart illustrating a main process of simulating the design of a radar system and operation of a navigation linkage by establishing a simulation environment for flight warfare linkage between an aircraft and a radar according to an embodiment of the present invention.

Advantages and features of the present invention, and a method of achieving them will become apparent with reference to the embodiments described below in detail together with the accompanying drawings. However, the present invention is not limited to the embodiments disclosed below, but may be implemented in various forms, and only these embodiments make the disclosure of the present invention complete, and those skilled in the art to which the present invention pertains. It is provided to fully inform the person of the scope of the invention, and the scope of the invention is only defined by the claims.

In describing the embodiments of the present invention, detailed descriptions of known functions or configurations will be omitted except when actually necessary in describing the embodiments of the present invention. In addition, terms to be described later are terms defined in consideration of functions in an embodiment of the present invention and may vary according to the intention or custom of users or operators. Therefore, the definition should be made based on the contents throughout this specification.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.

1 is an M&S (Modeling and Simulation) hierarchical diagram of an aircraft radar system, and shows the relationship between an aircraft and a radar in the aircraft M&S hierarchical diagram.

In the embodiment of the present invention, the relationship between aircraft M&S hierarchy and aircraft radar M&S was defined, and in order to simulate and verify radar operation at the aircraft system level, a system including flight warfare interlocking by extending engineering-grade radar M&S at the level of the existing sub-system We propose a level aircraft radar M&S environment.

2 is a conceptual diagram corresponding to a simulation apparatus according to an embodiment of the present invention to an aircraft system M&S hierarchy diagram.

Referring to FIG. 2, a radar simulation environment corresponds to an engineering-grade model at a sub-system level in an M&S hierarchy diagram, and a radar data processing and signal processing algorithm and architecture can be simulated.

Here, the aircraft radar system operation simulation can be implemented using a model-based software design technique such as UML (Unified Modeling Language) to simulate the configuration of the aircraft system including radar, the operation state of the radar, and the operation procedure. By including aviation linkage in the engineering level model, it is possible to implement a system level and engagement level M&S environment.

3 is a block diagram of an aircraft radar operation simulation apparatus according to an embodiment of the present invention. The simulation apparatus 300 includes a user interface unit 302, a navigation link simulation unit 304, and a radar system operation simulation unit 306. ), and a radar simulation execution unit 308. Here, the aircraft may be defined as, for example, a manned vehicle or an unmanned vehicle.

Referring to FIG. 3, the user interface unit 302 includes information required in a simulation process for verifying radar system operability and radar performance and function according to the user interface (eg, system radar operation command, scenario data, etc.). ) Can be set and input, and in real-time simulation, it can be implemented as an input means such as a flight controller for user's radar control, a cockpit including a screen, and a display means for displaying (display) the processing result of the radar operation simulation. have.

And, the navigation linkage simulation unit 304 is capable of performing a role such as overall control of the simulation of the aircraft (aircraft) of the flight equipment, and receives an operation command (control command) from the user interface 302 At the system level of the radar system operation simulation unit 306, a radar simulation execution unit that can play a role of linking the status and operation information of each component, and describes scenario data and radar operation commands for simulation of avionics equipment will be described later. It can provide functions such as sending to 308.

Here, the combat linkage simulation unit 304 may perform a combat class simulation with, for example, an enemy aircraft (enemy aircraft) by generating a simulated target scenario through an additional scenario input module (not shown).

In addition, the radar system operation simulation unit 306 can perform a function of simulating the operation of each component of the radar, the operation state of the radar, and the operation mode of the radar according to the control command from the navigation linkage simulation unit 304. , For this purpose, the radar system operation simulation unit 306 may have a configuration as shown in FIG. 4 as an example.

4 is a detailed block diagram of the radar system operation simulation unit shown in FIG. 3, wherein the radar system operation simulation unit 306 includes a power supply simulation unit 3062, an information transmission/reception simulation unit 3064, and an antenna simulation unit. 3066 and a radar signal processing simulation unit 3068.

4, the power supply simulation unit 3062 simulates power supply to the information transmission/reception simulation unit 3064, the antenna simulation unit 3066, and the radar signal processing simulation unit 3068 based on a power control command. And, it can perform functions such as transmitting its own state information to the radar signal processing simulation unit 3068.

Next, the information transmission/reception simulation unit 3064 generates simulation information for generating frequency signal waveform information suitable for various operating modes of the radar and its own state information, and transmits it to the radar preference processing simulation unit 3068. Can provide.

In addition, the antenna simulation unit 3066 generates antenna configuration information for applying the effect of the antenna to the beam radiation for the transmission signal and the signal received from the simulation target (not shown), and the generated antenna configuration information and its It is possible to provide a function such as transmitting the state information of the radar to the preference processing simulation unit 3068.

Here, the simulation of beam radiation for the simulation and application of the antenna effect may be performed by the radar simulation execution unit 308 of FIG. 3 to be described later.

In addition, the radar signal processing simulation unit 3068, simulation information provided from the power supply simulation unit 3062, the information transmission/reception simulation unit 3064, the antenna simulation unit 3066, etc., antenna configuration information, the state of each simulation unit Based on the information, it is possible to perform simulations on the operation check, operation state control, and operation mode of each component of the radar.

Here, the radar operation check may mean that the radar signal processing simulation unit 3068 performs a procedure for checking whether there is an abnormality in the avionics equipment at the system level. That is, the radar signal processing simulation unit 3068 may interwork with each component of the radar to simulate whether each component is powered on, a connection state, and a normal operation.

In addition, the operating state of the radar may be composed of a power-on step, a preparation step, an operation step, an operation failure step, and the like, which may mean that state control between these steps is performed.

In addition, the radar signal processing simulation unit 3068, for example, can selectively simulate each of the air-to-air, air-to-ground, and air-to-sea modes, control lower operation modes, and simulate transitions between each operation mode. Can provide.

In addition, the radar signal processing simulation unit 3068 controls the antenna, power supply, information transmission and reception, etc. in accordance with the control command received through interlocking with the flight combat linkage simulation unit 304 of FIG. 3, and controls the received radar simulation information. It can provide functions such as transmitting to interlocking equipment.

Referring back to FIG. 3, the radar simulation execution unit 308 simulates the antenna effect, detection performance, tracking performance, beam scheduling, etc. of the radar according to the radar operation state received from the flight combat linkage simulation unit 304. To this end, the radar simulation execution unit 308 may have a configuration as shown in FIG. 5 as an example.

FIG. 5 is a detailed block diagram of the radar simulation execution unit shown in FIG. 3, wherein the radar simulation execution unit 308 includes a control control simulation unit 3082, an antenna simulation unit 3084, and a signal processing simulation unit 3086. ), etc.

Referring to FIG. 5, the control control simulation unit 3082 may perform functions such as, for example, operating and implementing an operation mode of a radar, performing data processing for radar detection and tracking, and scheduling a radar beam. For this purpose, the control control simulation unit 3082 includes a detailed mode management model unit 3082-1, a search and tracking management model unit 3082-2, and a beam steering management model unit 3082-3. I can.

First, the detailed mode management model unit 3082-1 may perform functions such as operation and implementation of the operation mode with respect to the radar operation mode commanded by the radar system operation simulation unit 306 of FIG. 3.

As an example, when an air-to-air search and tracking mode is set in the user interface unit 302 according to the user interface, the detailed mode management model unit 3082-1 determines whether the mode can be executed, and a radar setting value according to the mode conversion. Changes, such as changing the beam steering method can be performed.

In addition, the search and tracking management model unit 3082-2 controls a radar search setting value including a search range suitable for each mode, a search pattern, a search period, a next search position, etc., and from the signal processing simulation unit 3086 The received target data may be used to perform a function of data processing for radar detection and tracking including target association, target tracking, and inter-beam processing.

In addition, the beam steering management model unit 3082-3 sets radar beam information to radiate the beam to the steering position determined by the search and tracking management model unit 3082-2, and sets the set information to the previously requested beam. It can perform functions such as periodic scheduling while managing together with steering requests.

Next, the antenna simulation unit 3084 may include, for example, an antenna pattern formation model unit 3084-1, by applying an antenna beam pattern according to the antenna steering direction requested by the control control simulation unit 3082 It can perform functions such as modeling the antenna effect on the gain and phase of the transmission and reception signals.

Meanwhile, the signal processing simulation unit 3086 performs functions such as self-speed compensation, pulse compression, and Doppler processing on the signal received through the antenna simulation unit 3084, and a range Doppler map through FFT (Fast Fourier Transform). It is capable of performing functions such as generating a (range-doppler map). For this purpose, the signal processing simulation unit 3086 includes an FFT execution model unit 3086-1 and a CFAR (Constant False Alarm Rate) execution model unit ( 3086-2), an angle calculation model unit 3086-3, an ambiguity removal model unit 3086-4, and the like.

First, the FFT performing model unit 3086-1 may perform a function such as generating a range Doppler map for estimating a target state by performing FFT on a received signal.

In addition, the CFAR execution model unit 3086-2 may perform a function such as extracting target information through the CFAR detector using the range Doppler map generated through the FFT execution model unit 309-86-1. .

In addition, the angle calculation model unit 3086-3 may perform a function such as calculating an angle with respect to the target through the value extracted through the CFAR execution model unit 3086-2, and the ambiguity removal model unit 3086 -4) can perform functions such as deriving the position and speed of the target by removing ambiguity based on the calculated angle, etc., and through these series of processes, the function of radar and Through performance analysis, it is possible to verify the design of the radar system and the operation of navigation linkage.

A series of processes for simulating the design of the radar system and the operation of the navigation linkage will be described in detail by using the apparatus for simulating the navigation linkage of this embodiment having the configuration as described above.

6 is a flow chart illustrating a main process of simulating the design of a radar system and operation of a navigation linkage by establishing a simulation environment for flight warfare linkage between an aircraft and a radar according to an embodiment of the present invention.

Referring to FIG. 6, the navigation linkage simulator 304 generates a control command for interlocking and simulating the state and motion information of each component at the radar system level according to an operation command received from the user interface 302. It transfers to the system operation simulation part 306 (step 602).

In response to this, the radar system operation simulation unit 306 simulates the operation check of each component of the radar according to the control command from the flight combat linkage simulation unit 304 (step 604), and then sends the simulation result to the avionics linkage simulation unit ( 304).

The navigation link simulation unit 304 generates a control command for checking the operation of the sub-system components of the radar and transmits the control command to the radar system operation simulation unit 306 (step 606).

Again, in the radar system operation simulation unit 306, the operation state of the radar is simulated according to the control command from the navigation linkage simulation unit 304 (step 608), and the operation mode according to the operation state of the radar is simulated (step 610). ), the simulation result is transmitted to the anti-war interlocking simulation unit 304 together with its own state information.

In response to this, the avionics interlocking simulator 304 generates scenario data and radar operation commands for simulating the avionics equipment based on the simulation of the operating state of the radar and the mode result of the operating mode according to each operating state, and the generated The data is transferred to the radar simulation execution unit 308 (step 612).

Thereafter, the radar simulation execution unit 308 simulates a search simulation and a target tracking simulation, that is, simulates the antenna effect, detection performance, and tracking performance of the radar according to the radar operation state (step 614), and the antenna requested from the control control simulation unit Through modeling that applies the antenna beam pattern according to the steering direction, the antenna effect on the gain and phase of the transmission and reception signals is generated (step 616), and target information is extracted using the range Doppler map generated through the FFT. Based on this, pilot data such as angle, position, and speed for the target signal are generated (step 618). According to an embodiment of the present invention, by executing a flight warfare link simulation between an aircraft and a radar through a series of such processes. It is possible to verify the design of the radar system and the operation of navigation linkage through the analysis of the function and performance of the radar.

Meanwhile, combinations of each block of the attached block diagram and each step of the flowchart may be performed by computer program instructions. Since these computer program instructions can be mounted on a processor of a general purpose computer, special purpose computer, or other programmable data processing equipment, the instructions executed by the processor of the computer or other programmable data processing equipment are shown in each block or flow chart of the block diagram. Each step creates a means to perform the functions described.

These computer program instructions can also be stored in a computer-usable or computer-readable memory, etc., which can be directed to a computer or other programmable data processing equipment to implement a function in a specific manner, so that the computer-usable or computer-readable memory It is also possible to produce an article of manufacture in which the instructions stored in the block diagram contain instruction means for performing the functions described in each block or flow chart.

In addition, since computer program instructions can be mounted on a computer or other programmable data processing equipment, a series of operation steps are performed on a computer or other programmable data processing equipment to create a process that is executed by a computer, It is also possible for the instructions to perform possible data processing equipment to provide steps for executing the functions described in each block of the block diagram and each step of the flowchart.

In addition, each block or each step may represent a module, segment, or part of code including at least one or more executable instructions for executing the specified logical function(s). In addition, it should be noted that in some alternative embodiments, functions mentioned in blocks or steps may occur out of order. For example, two blocks or steps shown in succession may in fact be performed substantially simultaneously, or the blocks or steps may sometimes be performed in the reverse order depending on the corresponding function.

The above description is merely illustrative of the technical idea of the present invention, and those of ordinary skill in the art to which the present invention pertains, various substitutions, modifications, and changes, etc., within the scope not departing from the essential characteristics of the present invention. It will be easy to see that this is possible. That is, the embodiments disclosed in the present invention are not intended to limit the technical idea of the present invention, but to explain the technical idea, and the scope of the technical idea of the present invention is not limited by these embodiments.

Accordingly, the scope of protection of the present invention should be interpreted by the claims to be described later, and all technical thoughts within the scope equivalent thereto should be interpreted as being included in the scope of the present invention.

302: user interface unit
304: anti-war linkage simulation unit
306: Radar system operation simulation unit
308: radar simulation execution unit
3062: power supply simulation unit
3064: Information transmission and reception simulation unit
3066, 3084: antenna simulation unit
3068: radar signal processing simulation unit
3082: control control simulation unit
3086: signal processing simulation unit

Claims (10)

A combat link simulation unit that links the state and motion information of each component of the radar at the level of the radar system according to the control command corresponding to the user interface, and generates scenario data and radar motion commands for simulation of the avionics equipment;
A radar system operation simulation unit that checks the operation of each component of the radar according to a control command from the navigation linkage simulation unit, simulates the operation state and operation mode of the radar, and transmits the simulation to the flight combat linkage simulation unit,
Including a radar simulation execution unit that simulates the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the operation state of the radar received from the flight combat linkage simulation unit.
A radar navigation link simulation device. The method of claim 1,
The radar system operation simulation unit,
An information transmission/reception simulation unit for generating simulation information for generating frequency signal waveform information suitable for each operating mode of the radar and its own state information,
An antenna simulation unit that generates antenna configuration information and its own state information for applying the effect of the antenna to the beam radiation for the transmission signal and the signal received from the simulated target,
Based on simulation information, antenna configuration information, and status information of each component provided from the information transmission/reception simulation unit and the antenna simulation unit, operation check of each component of the radar, operation state control, and operation mode are simulated. Including a radar signal processing simulation unit
A radar navigation link simulation device. The method of claim 2,
The radar signal processing simulation unit,
Air-to-air, air-to-ground, and air-to-sea modes can be selectively simulated
A radar navigation link simulation device. The method of claim 2,
The radar system operation simulation unit,
Further comprising a power supply simulation unit for simulating power supply to the information transmission/reception simulation unit, the antenna simulation unit, and the radar signal processing simulation unit based on a power control command, and transmitting status information of itself to the radar signal processing simulation unit.
A radar navigation link simulation device. The method of claim 1,
The radar simulation execution unit,
A control control simulation unit for scheduling the operation and implementation of the radar operation mode, data processing for detection and tracking of the radar, and a radar beam setting,
An antenna simulation unit for modeling an antenna effect on a gain and a phase of a transmission and reception signal by applying an antenna beam pattern according to an antenna steering direction requested from the control control simulation unit,
Comprising a signal processing simulation unit for performing self-speed compensation, pulse compression, and Doppler processing on the signal received through the antenna simulation unit, and generating a range-doppler map through Fast Fourier Transform (FFT).
A radar navigation link simulation device. The method of claim 5,
The control control simulation unit,
A detailed mode management model unit in charge of operation and implementation of an operation mode with respect to the radar operation mode commanded from the radar system operation simulation unit,
Controls the radar search setting value including the search range, search pattern, search period, and next search position of each mode, and includes target association, target tracking, and beam inter-beam processing using target data received from the signal processing simulation unit. A search and tracking management model unit that performs data processing for radar detection and tracking,
And a beam steering management model unit configured to set radar beam information to emit a beam to a steering position determined by the search and tracking management model unit, and perform periodic scheduling on the set information.
A radar navigation link simulation device. The method of claim 6,
The detailed mode management model unit,
When the air-to-air search and tracking mode is set according to the user interface, it determines whether the mode can be executed, changes the radar setting value according to the mode change, and changes the beam steering method.
A radar navigation link simulation device. The method of claim 5,
The signal processing simulation unit,
An FFT performance model unit for generating the range Doppler map for estimating a target state by performing the FFT on the received signal;
A CFAR execution model unit that extracts target information through a constant false alarm rate (CFAR) detector using the generated range Doppler map,
An angle calculation model unit that calculates an angle with respect to the target through the value extracted through the CFAR execution model unit,
Comprising a ambiguity removal model unit for deriving the position and speed of the target through ambiguity removal based on the calculated angle of the target
A radar navigation link simulation device. Generating scenario data and a radar operation command for simulating a radar navigation linkage based on a control command generated according to a user interface, and
Checking the operation of each component of the radar according to the generated control command, and simulating the operation state and operation mode of the radar,
Comprising the step of executing simulations for the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the operating state of the radar received through the simulating step
A method of simulating radar navigation. As a computer-readable recording medium storing a computer program that allows a processor to perform a radar motion-linked simulation method,
The avionics interlocking simulation method,
Generating scenario data and a radar operation command for simulating a radar navigation linkage based on a control command generated according to a user interface, and
Checking the operation of each component of the radar according to the generated control command, and simulating the operation state and operation mode of the radar,
Comprising the step of performing simulation for the antenna effect, detection performance, tracking performance, and beam scheduling of the radar according to the radar operation state received through the simulating step.
Computer-readable recording medium.

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