Simulation method, device and equipment of airborne radar target alarm display system

Abstract

The invention provides a simulation method, device and equipment for an airborne radar target alarm display system, and relates to the technical field of simulation, and the method comprises the steps: obtaining initial flight data corresponding to a plurality of simulation airplanes under the condition that a simulation self-inspection result corresponding to the airborne radar target alarm display simulation system is fault-free; target flight data corresponding to the simulation airplanes are determined based on the initial flight data; and performing simulation alarm display on a display interface of the airborne radar target alarm display simulation system based on the flight data of each target. According to the technical scheme, the complete working process of the airborne radar target alarm display system can be simulated without the help of semi-physical hardware equipment, the research cost for the airborne radar target alarm display system is reduced, the research efficiency is improved, and simulation can be carried out for multiple targets (namely simulation airplanes).

Description

Technical Field

[0001] The present invention relates to the field of simulation technology, and in particular to a simulation method, device and equipment for an airborne radar target warning display system. Background Art

[0002] The airborne radar target warning display system is an important avionics equipment, which is mainly used to improve the survivability and combat effectiveness of aircraft in complex electromagnetic environments.

[0003] In order to further develop the airborne radar target warning display technology, both domestic and foreign countries need to conduct in-depth research on the airborne radar target warning display system. However, under the existing technology, most of the research is based on semi-physical hardware equipment to simulate the airborne radar target warning display system, which is costly. In addition, the existing methods cannot conduct simulation research for special scenarios with multiple targets, and it is difficult to restore the complete workflow of the airborne radar target warning display system. Summary of the invention

[0004] The present invention provides a simulation method, device and equipment for an airborne radar target warning display system, which are used to solve the problems in the prior art that the airborne radar target warning display system is simulated based on semi-physical hardware equipment, the cost is high, and the prior art cannot perform simulation research on special scenarios with multiple targets, and it is also difficult to restore the complete workflow of the airborne radar target warning display system. The technical solution of the present invention can simulate the complete workflow of the airborne radar target warning display system without the aid of semi-physical hardware equipment, thereby reducing the research cost for the airborne radar target warning display system, improving the research efficiency, and can also perform simulation on multiple targets (i.e., simulated aircraft).

[0005] The present invention provides a simulation method for an airborne radar target warning display system, comprising the following steps.

[0006] When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, obtaining initial flight data corresponding to each of the plurality of simulated aircraft; Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

[0007] According to a simulation method of an airborne radar target warning display system provided by the present invention, the initial flight data includes an initial relative amplitude, and the target flight data includes a display relative amplitude; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft.

[0008] According to a simulation method for an airborne radar target warning display system provided by the present invention, the initial flight data includes an initial azimuth, and the target flight data includes a display azimuth; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft.

[0009] According to a simulation method for an airborne radar target warning display system provided by the present invention, the initial flight data includes an aircraft type processing value, and the target flight data includes an aircraft type; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the aircraft type corresponding to the simulated aircraft is determined based on the preset processing value interval within which the aircraft type processing value corresponding to the simulated aircraft lies.

[0010] According to a simulation method of an airborne radar target warning display system provided by the present invention, the method further includes: The initial relative amplitudes corresponding to the simulated aircraft are sorted in order, the simulated aircraft corresponding to the top K initial relative amplitudes are determined as high-priority simulated aircraft, and the remaining simulated aircraft are determined as low-priority simulated aircraft, wherein K is a positive integer.

[0011] According to a simulation method of an airborne radar target warning display system provided by the present invention, based on the flight data of each target, a simulated warning display is performed on a display interface of the airborne radar target warning display simulation system, comprising: Displaying the target flight data corresponding to each of the high-priority simulated aircraft on the display interface in a first simulation warning display mode; The target flight data corresponding to each of the low priority simulated aircraft are displayed on the display interface in accordance with the second simulation warning display mode.

[0012] According to a simulation method of an airborne radar target warning display system provided by the present invention, the method further includes: When a simulated power supply signal is received, or when a self-test instruction input by a user is received, a simulated self-test is performed to determine whether a simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0013] The present invention also provides a simulation device for an airborne radar target warning display system, comprising the following modules: An acquisition module is used to acquire initial flight data corresponding to a plurality of simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free; A determination module, used for respectively determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; The display module is used to perform simulated warning display on the display interface of the airborne radar target warning display simulation system based on the flight data of each target.

[0014] The present invention also provides an electronic device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein when the processor executes the computer program, a simulation method for an airborne radar target warning display system as described in any one of the above is implemented.

[0015] The present invention also provides a non-transitory computer-readable storage medium on which a computer program is stored. When the computer program is executed by a processor, the simulation method of the airborne radar target warning display system as described in any one of the above is implemented.

[0016] The present invention also provides a computer program product, comprising a computer program, wherein when the computer program is executed by a processor, the simulation method of the airborne radar target warning display system as described in any one of the above is implemented.

[0017] The simulation method, device and equipment of the airborne radar target warning display system provided by the present invention obtains initial flight data corresponding to multiple simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, determines the target flight data corresponding to each simulated aircraft respectively based on each initial flight data, and performs simulated warning display on the display interface of the airborne radar target warning display simulation system based on each target flight data. The technical solution of the present invention can simulate the complete workflow of the airborne radar target warning display system without the aid of semi-physical hardware equipment, reduces the research cost for the airborne radar target warning display system, improves the research efficiency, and can also simulate multiple targets (i.e., simulated aircraft). BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0019] Figure 1 It is a flow chart of a simulation method of an airborne radar target warning display system provided by the present invention.

[0020] Figure 2 It is a schematic diagram of the logical structure of the display interface provided by the present invention.

[0021] Figure 3 It is a structural schematic diagram of a simulation device for an airborne radar target warning display system provided by the present invention.

[0022] Figure 4 It is a structural schematic diagram of the electronic device provided by the present invention. DETAILED DESCRIPTION

[0023] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be clearly and completely described below in conjunction with the drawings of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0024] In view of the above problems in the prior art, the present invention provides a simulation method for an airborne radar target warning display system. Figure 1 FIG. 1 is a flow chart of a simulation method of an airborne radar target warning display system provided by the present invention, such as Figure 1 As shown, the method includes the following steps 110, 120 and 130.

[0025] Step 110: When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, initial flight data corresponding to a plurality of simulated aircraft are obtained.

[0026] Specifically, the present invention can simulate an airborne radar target warning display system of an aircraft (hereinafter referred to as a main aircraft), that is, an airborne radar target warning display simulation system, and can perform a simulated self-check, which is a self-check of the airborne radar target warning display simulation system. When the simulated self-check result corresponding to the airborne radar target warning display simulation system is fault-free, the initial flight data corresponding to multiple simulated aircraft are obtained. The multiple simulated aircraft can be multiple simulated aircraft within the simulated radar range corresponding to the main aircraft. It is easy to understand that since the present invention is a simulation method, the initial flight data corresponding to the multiple simulated aircraft can be obtained from a pre-set database.

[0027] In one embodiment, the method further comprises: When a simulated power supply signal is received, or when a self-test instruction input by a user is received, a simulated self-test is performed to determine whether a simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0028] Specifically, it can be pre-set to receive a simulated power supply signal when the method is executed, and the user can also input a self-test instruction as needed. A simulated self-test can be performed when a simulated power supply signal is received, or when a self-test instruction input by the user is received, that is, a simulated self-test can be performed on the data corresponding to the airborne radar target warning display simulation system to determine whether the simulated self-test result is fault-free or whether the simulated self-test result is faulty. The subject aircraft data can be pre-set as needed, and the embodiments of the present invention are not specifically limited here. For example, when it is necessary to study the airborne radar target warning display system of a certain A aircraft, the subject aircraft data can be set to the characteristic data of various aspects of a certain A aircraft.

[0029] In the above embodiment, when a simulated power supply signal is received, or when a self-test instruction input by a user is received, a simulated self-test is performed to determine whether the simulated self-test result is fault-free or faulty. The power-on self-test process of the airborne radar target warning display system is restored, which facilitates the study of the airborne radar target warning display system.

[0030] Step 120: Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data.

[0031] Specifically, the target flight data corresponding to each simulated aircraft can be determined based on each initial flight data. It should be noted that the initial flight data simulates the actual flight data of other aircraft obtained by the aircraft during the flight, and the initial flight data may include an initial relative amplitude, an initial azimuth, and an aircraft type processing value. The target flight data simulates the data displayed on the airborne radar target warning display system based on the actual flight data, and the target flight data may include a display relative amplitude, a display azimuth, and an aircraft type.

[0032] In one embodiment, the initial flight data includes an initial relative amplitude, and the target flight data includes a displayed relative amplitude; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft.

[0033] Specifically, the initial flight data may include the initial relative amplitude , target flight data including display of relative amplitude For each simulated aircraft, the display relative amplitude corresponding to the simulated aircraft can be determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft. , the above process can be expressed by the following formula:

[0034] in, Indicates the number of the simulated aircraft. Indicates the canvas size corresponding to the display interface. Indicates the maximum preset amplitude.

[0035] In the above embodiment, for each simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft. The display relative amplitude is applicable to the relative amplitude of the display interface and can more accurately simulate the display of relative amplitude by the airborne radar target warning display system.

[0036] In one embodiment, the initial flight data includes an initial azimuth, and the target flight data includes a display azimuth; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft.

[0037] Specifically, the initial flight data includes an initial azimuth, and the target flight data includes a display azimuth. For each simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft. The above process can be expressed by the following formula:

[0038] in, Indicates simulated aircraft The corresponding display azimuth, Indicates simulated aircraft The corresponding initial azimuth. It should be noted that the remark information of the airborne radar target warning display system will display the azimuth of each aircraft in the radar, but because the angles sent by other aircraft are obtained, it is necessary to invert them to determine the azimuth that the main aircraft needs to display.

[0039] In the above embodiment, for each simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft, which can more accurately simulate the display of the azimuth by the airborne radar target warning display system.

[0040] In one embodiment, the initial flight data includes an aircraft type processing value, and the target flight data includes an aircraft type; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the aircraft type corresponding to the simulated aircraft is determined based on the preset processing value interval within which the aircraft type processing value corresponding to the simulated aircraft lies.

[0041] Specifically, the initial flight data includes an aircraft type processing value, and the target flight data includes an aircraft type. For each simulated aircraft, the aircraft type corresponding to the simulated aircraft can be determined based on the preset processing value interval in which the aircraft type processing value corresponding to the simulated aircraft is located. There can be multiple preset processing value intervals, and the ranges corresponding to each preset processing value interval can be set as needed, which is not specifically limited in the embodiment of the present invention.

[0042] For example, simulated aircraft Corresponding aircraft type It can be determined by the following formula:

[0043] in, Indicates simulated aircraft The corresponding aircraft type processing value, , , 3 and Both represent aircraft types, and , , 3 and The aircraft types represented are different. Aircraft types may include helicopters, for example.

[0044] In the above embodiment, for each simulated aircraft, the aircraft type corresponding to the simulated aircraft can be determined based on the preset processing value interval of the aircraft type processing value corresponding to the simulated aircraft, which can more accurately simulate the display of the aircraft type by the airborne radar target warning display system.

[0045] In one embodiment, the method further comprises: The initial relative amplitudes corresponding to the simulated aircraft are sorted in order, the simulated aircraft corresponding to the top K initial relative amplitudes are determined as high-priority simulated aircraft, and the remaining simulated aircraft are determined as low-priority simulated aircraft, wherein K is a positive integer.

[0046] Specifically, the initial relative amplitudes corresponding to the simulated aircraft can be sorted by size, and the simulated aircraft corresponding to the top K initial relative amplitudes can be determined as high-priority simulated aircraft, and the remaining simulated aircraft can be determined as low-priority simulated aircraft, where K is a positive integer, for example, K can be 1, and K can also be 5. It is easy to understand that the priority can represent the distance from the simulated aircraft to the main aircraft, and the high-priority simulated aircraft is closer to the main aircraft than the low-priority simulated aircraft.

[0047] In the above embodiment, the initial relative amplitudes corresponding to the simulated aircraft are sorted by size, and the simulated aircraft corresponding to the top K initial relative amplitudes are determined as high-priority simulated aircraft, and the remaining simulated aircraft are determined as low-priority simulated aircraft, so as to facilitate the subsequent different displays of target flight data corresponding to simulated aircraft of different priorities.

[0048] Step 130: Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

[0049] Specifically, a simulated warning display can be performed on the display interface of the airborne radar target warning display simulation system based on each target flight data, for example, the simulated aircraft corresponding to each target flight data is displayed at the corresponding position of the display interface. The icon corresponding to the simulated aircraft can also be displayed at the display position corresponding to the simulated aircraft, and the display relative amplitude and display azimuth are used to determine the display position of the simulated aircraft on the display interface, and the aircraft type is used to determine the icon of the simulated aircraft on the display interface, and then the simulated warning display is performed on the display interface based on the display position corresponding to each simulated aircraft. In addition, the time for performing the simulated warning display can be determined according to the time corresponding to the initial flight data. For example, if the initial flight data is data obtained at 18:36:00, the simulated warning display can be performed on the display interface based on the target flight data corresponding to the initial flight data within 18:36:00 to 18:36:10.

[0050] Optionally, Figure 2 is a schematic diagram of the logical structure of the display interface provided by the present invention, such as Figure 2 As shown in the figure, the display interface can be divided into three levels in terms of logical structure, namely, the presentation layer, the business logic layer and the data access layer. The data access layer is used to obtain and update the target flight data corresponding to each simulated aircraft, the business logic layer is used to process each target flight data before display, and the presentation layer is used for simulation warning display and user interaction.

[0051] In one embodiment, the simulated warning display is performed on the display interface of the airborne radar target warning display simulation system based on the flight data of each target, including: Displaying the target flight data corresponding to each of the high-priority simulated aircraft on the display interface in a first simulation warning display mode; The target flight data corresponding to each of the low priority simulated aircraft are displayed on the display interface in accordance with the second simulation warning display mode.

[0052] Specifically, the target flight data corresponding to each high-priority simulated aircraft can be displayed on the display interface according to the first simulation alarm display mode. For example, the first simulation alarm display mode can be flashing, and then the target flight data corresponding to the high-priority simulated aircraft can be flashing on the display interface. The target flight data corresponding to each low-priority simulated aircraft can also be displayed on the display interface according to the second simulation alarm display mode. For example, the second simulation alarm display mode can be always on, and then the target flight data corresponding to the low-priority simulated aircraft can be always on on the display interface. Among them, the first simulation alarm display mode and the second simulation alarm display mode can be set as needed. For example, in addition to flashing and always on, they can also be set to change the display color and change the display size, etc. The embodiment of the present invention is not specifically limited here.

[0053] In the above embodiment, the target flight data corresponding to each high-priority simulated aircraft is displayed on the display interface according to the first simulation warning display mode, and the target flight data corresponding to each low-priority simulated aircraft is displayed on the display interface according to the second simulation warning display mode. The workflow of the airborne radar target warning display system for performing different displays for different aircraft is accurately simulated.

[0054] The simulation method of the airborne radar target warning display system provided by the present invention obtains initial flight data corresponding to a plurality of simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, determines target flight data corresponding to each simulated aircraft respectively based on each initial flight data, and performs simulated warning display on the display interface of the airborne radar target warning display simulation system based on each target flight data. The technical solution of the present invention can simulate the complete workflow of the airborne radar target warning display system without the aid of semi-physical hardware equipment, reduces the research cost for the airborne radar target warning display system, improves the research efficiency, and can also simulate multiple targets (i.e., simulated aircraft).

[0055] The simulation device of the airborne radar target warning display system provided by the present invention is described below. The simulation device of the airborne radar target warning display system described below and the simulation method of the airborne radar target warning display system described above can be referred to each other.

[0056] Figure 3 FIG. 1 is a schematic diagram of the structure of a simulation device for an airborne radar target warning display system provided by the present invention. Figure 3 As shown, the simulation device 300 of the airborne radar target warning display system includes the following modules: The acquisition module 310 is used to acquire initial flight data corresponding to a plurality of simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free; A determination module 320, configured to determine target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; The display module 330 is used to perform simulated warning display on the display interface of the airborne radar target warning display simulation system based on the flight data of each target.

[0057] In one embodiment, the initial flight data includes an initial relative amplitude, the target flight data includes a display relative amplitude, and the determination module 320 is specifically configured to: For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft.

[0058] In one embodiment, the initial flight data includes an initial azimuth, the target flight data includes a display azimuth, and the determination module 320 is further configured to: For each of the simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft.

[0059] In one embodiment, the initial flight data includes an aircraft type processing value, the target flight data includes an aircraft type, and the determination module 320 is further configured to: For each of the simulated aircraft, the aircraft type corresponding to the simulated aircraft is determined based on the preset processing value interval within which the aircraft type processing value corresponding to the simulated aircraft lies.

[0060] In one embodiment, the simulation device of the airborne radar target warning display system further includes a priority module, which is specifically used to: The initial relative amplitudes corresponding to the simulated aircraft are sorted in order, the simulated aircraft corresponding to the top K initial relative amplitudes are determined as high-priority simulated aircraft, and the remaining simulated aircraft are determined as low-priority simulated aircraft, wherein K is a positive integer.

[0061] In one embodiment, the display module 330 is specifically used for: Displaying the target flight data corresponding to each of the high-priority simulated aircraft on the display interface in a first simulation warning display mode; The target flight data corresponding to each of the low priority simulated aircraft are displayed on the display interface in accordance with the second simulation warning display mode.

[0062] In one embodiment, the simulation device of the airborne radar target warning display system further includes a self-checking module, which is specifically used to: When a simulated power supply signal is received, or when a self-test instruction input by a user is received, a simulated self-test is performed to determine whether a simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0063] The simulation device of the airborne radar target warning display system provided by the present invention obtains initial flight data corresponding to a plurality of simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, determines target flight data corresponding to each simulated aircraft respectively based on each initial flight data, and performs simulated warning display on the display interface of the airborne radar target warning display simulation system based on each target flight data. The technical solution of the present invention can simulate the complete workflow of the airborne radar target warning display system without the aid of semi-physical hardware equipment, reduces the research cost for the airborne radar target warning display system, improves the research efficiency, and can also simulate multiple targets (i.e., simulated aircraft).

[0064] Figure 4 An example of a physical structure diagram of an electronic device is shown in FIG. Figure 4 As shown, the electronic device may include: a processor 410, a communications interface 420, a memory 430 and a communication bus 440, wherein the processor 410, the communications interface 420 and the memory 430 communicate with each other through the communication bus 440. The processor 410 may call the logic instructions in the memory 430 to execute the simulation method of the airborne radar target warning display system, and the method includes: When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, obtaining initial flight data corresponding to each of the plurality of simulated aircraft; Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

[0065] In addition, the logic instructions in the above-mentioned memory 430 can be implemented in the form of a software functional unit and can be stored in a computer-readable storage medium when it is sold or used as an independent product. Based on this understanding, the technical solution of the present invention, in essence, or the part that contributes to the prior art or the part of the technical solution, can be embodied in the form of a software product, and the computer software product is stored in a storage medium, including a number of instructions for a computer device (which can be a personal computer, a server, or a network device, etc.) to perform all or part of the steps of the method described in each embodiment of the present invention. The aforementioned storage medium includes: U disk, mobile hard disk, read-only memory (ROM, Read-Only Memory), random access memory (RAM, Random Access Memory), disk or optical disk, etc. Various media that can store program codes.

[0066] On the other hand, the present invention further provides a computer program product, the computer program product includes a computer program, the computer program can be stored on a non-transitory computer-readable storage medium, when the computer program is executed by a processor, the computer can execute the simulation method of the airborne radar target warning display system provided by the above methods, the method includes: When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, obtaining initial flight data corresponding to each of the plurality of simulated aircraft; Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

[0067] In another aspect, the present invention further provides a non-transitory computer-readable storage medium having a computer program stored thereon, which is implemented when the computer program is executed by a processor to perform the simulation method of the airborne radar target warning display system provided by the above methods, the method comprising: When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, obtaining initial flight data corresponding to each of the plurality of simulated aircraft; Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

[0068] The device embodiments described above are merely illustrative, wherein the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, they may be located in one place, or they may be distributed on multiple network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the scheme of this embodiment. Ordinary technicians in this field can understand and implement it without paying creative labor.

[0069] Through the description of the above implementation methods, those skilled in the art can clearly understand that each implementation method can be implemented by means of software plus a necessary general hardware platform, and of course, can also be implemented by hardware. Based on this understanding, the above technical solution is essentially or the part that contributes to the prior art can be embodied in the form of a software product, and the computer software product can be stored in a computer-readable storage medium, such as ROM / RAM, a disk, an optical disk, etc., including a number of instructions for a computer device (which can be a personal computer, a server, or a network device, etc.) to execute the methods described in each embodiment or some parts of the embodiments.

[0070] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A simulation method for an airborne radar target warning display system, characterized in that: include: When the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free, obtaining initial flight data corresponding to each of the plurality of simulated aircraft; Determine the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; Based on the flight data of each target, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system.

2. The simulation method of the airborne radar target warning display system according to claim 1, characterized in that: The initial flight data includes an initial relative amplitude, and the target flight data includes a display relative amplitude; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on the preset maximum amplitude, the canvas size corresponding to the display interface and the initial relative amplitude corresponding to the simulated aircraft.

3. The simulation method of the airborne radar target warning display system according to claim 1, characterized in that: The initial flight data includes an initial azimuth, and the target flight data includes a display azimuth; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the negative value of the initial azimuth corresponding to the simulated aircraft is determined as the display azimuth corresponding to the simulated aircraft.

4. The simulation method of the airborne radar target warning display system according to claim 1, characterized in that: The initial flight data includes an aircraft type processing value, and the target flight data includes an aircraft type; The step of respectively determining the target flight data corresponding to each of the simulated aircraft based on each of the initial flight data comprises: For each of the simulated aircraft, the aircraft type corresponding to the simulated aircraft is determined based on the preset processing value interval within which the aircraft type processing value corresponding to the simulated aircraft lies.

5. The simulation method of the airborne radar target warning display system according to claim 2, characterized in that: The method further comprises: The initial relative amplitudes corresponding to the simulated aircraft are sorted in order, the simulated aircraft corresponding to the top K initial relative amplitudes are determined as high-priority simulated aircraft, and the remaining simulated aircraft are determined as low-priority simulated aircraft, wherein K is a positive integer.

6. The simulation method of the airborne radar target warning display system according to claim 5, characterized in that: The simulated warning display is performed on the display interface of the airborne radar target warning display simulation system based on the flight data of each target, including: Displaying the target flight data corresponding to each of the high-priority simulated aircraft on the display interface in a first simulation warning display mode; The target flight data corresponding to each of the low priority simulated aircraft are displayed on the display interface in accordance with the second simulation warning display mode.

7. The simulation method of the airborne radar target warning display system according to any one of claims 1 to 6, characterized in that: The method further comprises: When a simulated power supply signal is received, or when a self-test instruction input by a user is received, a simulated self-test is performed to determine whether a simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

8. A simulation device for an airborne radar target warning display system, characterized in that: include: An acquisition module is used to acquire initial flight data corresponding to a plurality of simulated aircraft respectively when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free; A determination module, used for respectively determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; The display module is used to perform simulated warning display on the display interface of the airborne radar target warning display simulation system based on the flight data of each target.

9. An electronic device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein: When the processor executes the computer program, the simulation method of the airborne radar target warning display system according to any one of claims 1 to 7 is implemented.

10. A non-transitory computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, a simulation method for an airborne radar target warning display system as claimed in any one of claims 1 to 7 is implemented.

Images