Simulation method, device and equipment for airborne radar target warning display system

Abstract

The present invention provides a simulation method, device, and apparatus for an airborne radar target warning display system, relating to the field of simulation technology. The method comprises: obtaining initial flight data corresponding to multiple simulated aircraft when a simulated self-test result corresponding to the airborne radar target warning display simulation system indicates no faults; determining target flight data corresponding to each simulated aircraft based on the initial flight data; and displaying a simulated warning on a display interface of the airborne radar target warning display simulation system based on the target flight data. The technical solution of the present invention can simulate the complete workflow of an airborne radar target warning display system without the need for hardware-in-the-loop (HIL) equipment, thereby reducing research costs and improving research efficiency for the airborne radar target warning display system. Furthermore, the method can simulate multiple targets (i.e., simulated aircraft).

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, mainly used to improve the survivability and combat effectiveness of aircraft in complex electromagnetic environments.

[0003] To further develop airborne radar target warning display technology, in-depth research on airborne radar target warning display systems is needed both domestically and internationally. However, with existing technologies, most research relies on hardware-in-the-loop simulations of airborne radar target warning display systems, which is costly. Furthermore, existing methods are unable to simulate the unique multi-target scenario and struggle to recreate the complete workflow of an 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 defects of the prior art in which the airborne radar target warning display system is simulated based on semi-physical hardware equipment, which is costly, cannot be simulated for special scenarios with multiple targets, and is 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 help of semi-physical hardware equipment, thereby reducing the research cost for the airborne radar target warning display system and improving the research efficiency. In addition, the system can also simulate 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;

[0007] Determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0008] 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.

[0009] 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;

[0010] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0011] For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on a preset maximum amplitude value, a canvas size corresponding to the display interface, and an initial relative amplitude corresponding to the simulated aircraft.

[0012] 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 azimuth, and the target flight data includes a display azimuth;

[0013] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0014] For each simulated aircraft, the negative value of the initial azimuth angle corresponding to the simulated aircraft is determined as the display azimuth angle corresponding to the simulated aircraft.

[0015] 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;

[0016] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0017] 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.

[0018] According to a simulation method of an airborne radar target warning display system provided by the present invention, the method further includes:

[0019] The initial relative amplitudes corresponding to the simulated aircraft are sorted by size, 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.

[0020] 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:

[0021] 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;

[0022] 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.

[0023] According to a simulation method of an airborne radar target warning display system provided by the present invention, the method further includes:

[0024] 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 corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0025] The present invention also provides a simulation device for an airborne radar target warning display system, comprising the following modules:

[0026] An acquisition module is used to acquire initial flight data corresponding to a plurality of simulated aircraft respectively when a simulation self-test result corresponding to the airborne radar target warning display simulation system is fault-free;

[0027] a determination module, configured to determine target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0028] 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.

[0029] 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. When the processor executes the computer program, a simulation method for an airborne radar target warning display system as described above is implemented.

[0030] The present invention also provides a non-transitory computer-readable storage medium having a computer program stored thereon. 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.

[0031] 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.

[0032] The present invention provides a simulation method, apparatus, and device for an airborne radar target warning display system. When the simulated self-test results for the airborne radar target warning display simulation system indicate no faults, the method obtains initial flight data corresponding to multiple simulated aircraft, determines target flight data corresponding to each simulated aircraft based on the initial flight data, and then displays a simulated warning on the display interface of the airborne radar target warning display simulation system based on the target flight data. This technical solution can simulate the complete workflow of an airborne radar target warning display system without the need for hardware-in-the-loop (HIL) hardware, reducing research costs and improving research efficiency. Furthermore, it can simulate multiple targets (i.e., simulated aircraft). BRIEF DESCRIPTION OF THE DRAWINGS

[0033] In order to more clearly illustrate the technical solutions in the present invention or the prior art, a brief introduction is given below to 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 any creative work.

[0034] Figure 1 It is a flow chart of a simulation method of an airborne radar target warning display system provided by the present invention.

[0035] Figure 2 It is a schematic diagram of the logical structure of the display interface provided by the present invention.

[0036] Figure 3 It is a structural schematic diagram of a simulation device of an airborne radar target warning display system provided by the present invention.

[0037] Figure 4 It is a structural schematic diagram of the electronic device provided by the present invention. DETAILED DESCRIPTION

[0038] To make the objectives, technical solutions, and advantages of the present invention more clear, the technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the embodiments described are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts shall fall within the scope of protection of the present invention.

[0039] 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, as shown in FIG. Figure 1As shown, the method includes the following steps 110, 120 and 130.

[0040] 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 each of the plurality of simulated aircraft are obtained.

[0041] Specifically, the present invention can simulate the airborne radar target warning display system of an aircraft (hereinafter referred to as the subject aircraft), namely, the airborne radar target warning display simulation system, and perform a simulated self-test. This simulated self-test is a self-test of the airborne radar target warning display simulation system. If the simulated self-test results of the airborne radar target warning display simulation system are normal, 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 subject aircraft. As will be readily understood, 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.

[0042] In one embodiment, the method further comprises:

[0043] 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 corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0044] 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. When a simulated power supply signal is received, or when a self-test instruction input by the user is received, a simulated self-test can be performed, 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 embodiment of the present invention does not make specific limitations 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 the certain A aircraft.

[0045] In the above embodiment, upon receiving a simulated power supply signal or a user-input self-test command, a simulated self-test is performed to determine whether the simulated self-test result is fault-free or faulty. This restores the power-on self-test process of the airborne radar target warning display system, facilitating research on the airborne radar target warning display system.

[0046] Step 120: Determine target flight data corresponding to each simulated aircraft based on each of the initial flight data.

[0047] Specifically, 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 acquired by an aircraft during flight. The initial flight data may include initial relative amplitude, initial azimuth, and aircraft type processing values. The target flight data simulates the data displayed on the airborne radar target warning display system based on the actual flight data. The target flight data may include display relative amplitude, display azimuth, and aircraft type.

[0048] In one embodiment, the initial flight data includes an initial relative amplitude, and the target flight data includes a display relative amplitude;

[0049] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0050] For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on a preset maximum amplitude value, a canvas size corresponding to the display interface, and an initial relative amplitude corresponding to the simulated aircraft.

[0051] Specifically, the initial flight data may include the initial relative amplitude , target flight data including display 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:

[0052]

[0053] in, Indicates the number of the simulated aircraft, Indicates the canvas size corresponding to the display interface. Indicates the maximum preset amplitude.

[0054] 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 the relative amplitude by the airborne radar target warning display system.

[0055] In one embodiment, the initial flight data includes an initial azimuth, and the target flight data includes a display azimuth;

[0056] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0057] For each simulated aircraft, the negative value of the initial azimuth angle corresponding to the simulated aircraft is determined as the display azimuth angle corresponding to the simulated aircraft.

[0058] Specifically, the initial flight data includes the initial azimuth, and the target flight data includes the 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:

[0059]

[0060] 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 it obtains the angles sent by other aircraft, it needs to be inverted to determine the azimuth that the main aircraft needs to display.

[0061] In the above embodiment, for each simulated aircraft, the negative value of the initial azimuth angle corresponding to the simulated aircraft is determined as the display azimuth angle corresponding to the simulated aircraft, which can more accurately simulate the display of azimuth angles by the airborne radar target warning display system.

[0062] In one embodiment, the initial flight data includes an aircraft type processing value, and the target flight data includes an aircraft type;

[0063] The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes:

[0064] 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.

[0065] 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 within which the aircraft type processing value corresponding to the simulated aircraft falls. Multiple preset processing value intervals can be provided, and the range corresponding to each preset processing value interval can be set as needed, which is not specifically limited in this embodiment of the present invention.

[0066] For example, simulated aircraft Corresponding aircraft type It can be determined by the following formula:

[0067]

[0068] 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.

[0069] 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 range 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.

[0070] In one embodiment, the method further comprises:

[0071] The initial relative amplitudes corresponding to the simulated aircraft are sorted by size, 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.

[0072] 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 or K can be 5. It is easy to understand that the priority can represent the distance between the simulated aircraft and the main aircraft, and the high-priority simulated aircraft are closer to the main aircraft than the low-priority simulated aircraft.

[0073] 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 different displays of target flight data corresponding to simulated aircraft of different priorities.

[0074] 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.

[0075] Specifically, a simulated warning display can be performed on the display interface of the airborne radar target warning display simulation system based on the flight data of each target. For example, the simulated aircraft corresponding to each target flight data is displayed at the corresponding position on the display interface. An icon corresponding to the simulated aircraft can also be displayed at the display position corresponding to the simulated aircraft. 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. Then, a simulated warning display is performed on the display interface for the icon based on the display position corresponding to each simulated aircraft. In addition, the time for performing the simulated warning display can be determined based on the time corresponding to the initial flight data. For example, if the initial flight data is obtained at 18:36:00, a simulated warning display can be performed on the display interface based on the target flight data corresponding to the initial flight data between 18:36:00 and 18:36:10.

[0076] Optionally, Figure 2 This 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 logically divided into three layers: 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 simulated warning display and user interaction.

[0077] In one embodiment, performing a simulated warning display on a display interface of the airborne radar target warning display simulation system based on the flight data of each target includes:

[0078] 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;

[0079] 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.

[0080] 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 does not make specific limitations here.

[0081] In the above embodiment, the display interface displays target flight data corresponding to each high-priority simulated aircraft in a first simulated warning display mode, while the display interface displays target flight data corresponding to each low-priority simulated aircraft in a second simulated warning display mode. This accurately simulates the workflow of the airborne radar target warning display system, which provides different displays for different aircraft.

[0082] The simulation method for an airborne radar target warning display system provided by the present invention obtains initial flight data corresponding to multiple simulated aircraft when the simulated self-test results of the airborne radar target warning display simulation system indicate no faults. Based on the initial flight data, target flight data corresponding to each simulated aircraft is determined. Based on the target flight data, a simulated warning display is performed on the display interface of the airborne radar target warning display simulation system. This technical solution can simulate the complete workflow of an airborne radar target warning display system without the need for hardware-in-the-loop (HIL) equipment, reducing research costs and improving research efficiency for the airborne radar target warning display system. Furthermore, it can simulate multiple targets (i.e., simulated aircraft).

[0083] 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 referenced to each other.

[0084] 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:

[0085] An acquisition module 310 is configured to acquire initial flight data corresponding to each of the plurality of simulated aircraft when the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free;

[0086] A determination module 320 is configured to determine target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0087] 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.

[0088] In one embodiment, the initial flight data includes an initial relative amplitude, and the target flight data includes a display relative amplitude. The determination module 320 is specifically configured to:

[0089] For each of the simulated aircraft, the display relative amplitude corresponding to the simulated aircraft is determined based on a preset maximum amplitude value, a canvas size corresponding to the display interface, and an initial relative amplitude corresponding to the simulated aircraft.

[0090] In one embodiment, the initial flight data includes an initial azimuth, and the target flight data includes a display azimuth. The determination module 320 is further configured to:

[0091] For each simulated aircraft, the negative value of the initial azimuth angle corresponding to the simulated aircraft is determined as the display azimuth angle corresponding to the simulated aircraft.

[0092] 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:

[0093] 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.

[0094] In one embodiment, the simulation device of the airborne radar target warning display system further includes a priority module, which is specifically used to:

[0095] The initial relative amplitudes corresponding to the simulated aircraft are sorted by size, 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.

[0096] In one embodiment, the display module 330 is specifically configured to:

[0097] 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;

[0098] 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.

[0099] In one embodiment, the simulation device of the airborne radar target warning display system further includes a self-test module, which is specifically used to:

[0100] 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 corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

[0101] The simulation device for an airborne radar target warning display system provided by the present invention obtains initial flight data corresponding to multiple simulated aircraft, when the simulated self-test results of the airborne radar target warning display simulation system indicate no faults. Based on the initial flight data, the device determines target flight data corresponding to each simulated aircraft. Based on the target flight data, the device then simulates a warning on the display interface of the airborne radar target warning display simulation system. This technical solution can simulate the complete workflow of an airborne radar target warning display system without the need for hardware-in-the-loop (HIL) equipment, reducing research costs and improving research efficiency for the system. Furthermore, the system can simulate multiple targets (i.e., simulated aircraft).

[0102] Figure 4 An example of a physical structure diagram of an electronic device is shown below. 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 via the communication bus 440. The processor 410 may call the logic instructions in the memory 430 to execute a simulation method for an airborne radar target warning display system, the method including:

[0103] 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;

[0104] Determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0105] 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.

[0106] Furthermore, the logic instructions in the aforementioned memory 430 can be implemented as software functional units and, when sold or used as independent products, can be stored in a computer-readable storage medium. Based on this understanding, the technical solution of the present invention, or the portion that contributes to the prior art, or a portion of the technical solution, can be embodied in the form of a software product. This computer software product, stored in a storage medium, includes instructions for enabling a computer device (which can be a personal computer, server, or network device, etc.) to perform all or part of the steps of the methods described in various embodiments of the present invention. The aforementioned storage medium includes various media capable of storing program code, such as a USB flash drive, a mobile hard drive, a read-only memory (ROM), a random access memory (RAM), a magnetic disk, or an optical disk.

[0107] On the other hand, the present invention further provides a computer program product, comprising a computer program. The computer program may be stored on a non-transitory computer-readable storage medium. When the computer program is executed by a processor, the computer can perform the simulation method of the airborne radar target warning display system provided by the above methods, the method comprising:

[0108] 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;

[0109] Determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0110] 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.

[0111] In another aspect, the present invention further provides a non-transitory computer-readable storage medium having a computer program stored thereon. When the computer program is executed by a processor, the method for simulating an airborne radar target warning display system provided by the above methods is implemented, the method comprising:

[0112] 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;

[0113] Determining target flight data corresponding to each of the simulated aircraft based on each of the initial flight data;

[0114] 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.

[0115] The device embodiments described above are merely illustrative. The units described as separate components may or may not be physically separate, and the components shown as units may or may not be physical units, i.e., they may be located in one location or distributed across multiple network units. Some or all of the modules may be selected based on actual needs to achieve the objectives of the present embodiment. Persons of ordinary skill in the art will be able to understand and implement the present invention without inventive effort.

[0116] Through the above description of the embodiments, those skilled in the art will clearly understand that each embodiment can be implemented using software plus a necessary general-purpose hardware platform, or of course, hardware. Based on this understanding, the essence of the above technical solution, or the portion that contributes to the prior art, can be embodied in the form of a software product. This computer software product can be stored in a computer-readable storage medium, such as ROM / RAM, a magnetic disk, or an optical disk, and includes a number of instructions for causing a computer device (such as a personal computer, server, or network device) to execute the methods described in each embodiment or certain portions of the embodiments.

[0117] 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 various 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; Determining 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; The initial flight data includes an initial relative amplitude, and the target flight data includes a display relative amplitude; The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes: For each simulated aircraft, 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 corresponding to the simulated aircraft is determined by the following formula: Among them, F R Indicates the relative amplitude of the display corresponding to the simulated aircraft R, R represents the number of the simulated aircraft, C Max Indicates the canvas size corresponding to the display interface, T Max Indicates the maximum preset amplitude, T R represents the initial relative amplitude corresponding to the simulated aircraft R.

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 azimuth, and the target flight data includes a display azimuth; The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes: For each simulated aircraft, the negative value of the initial azimuth angle corresponding to the simulated aircraft is determined as the display azimuth angle 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 aircraft type processing value, and the target flight data includes an aircraft type; The determining of target flight data corresponding to each simulated aircraft based on each of the initial flight data includes: 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.

4. The simulation method of the airborne radar target warning display system according to claim 1, characterized in that: The method further comprises: The initial relative amplitudes corresponding to the simulated aircraft are sorted by size, 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.

5. The simulation method of the airborne radar target warning display system according to claim 4, 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.

6. The simulation method of the airborne radar target warning display system according to any one of claims 1 to 5, 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 the simulated self-test result corresponding to the airborne radar target warning display simulation system is fault-free or faulty.

7. 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 a simulation self-test result corresponding to the airborne radar target warning display simulation system is fault-free; a determination module, configured to determine target flight data corresponding to each of the simulated aircraft based on each of the initial flight data; A display module is used to perform a simulated warning display on a display interface of the airborne radar target warning display simulation system based on the flight data of each target; The initial flight data includes an initial relative amplitude, the target flight data includes a display relative amplitude, and the determination module is specifically configured to: For each simulated aircraft, 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 corresponding to the simulated aircraft is determined by the following formula: Among them, F R Indicates the relative amplitude of the display corresponding to the simulated aircraft R, R represents the number of the simulated aircraft, C Max Indicates the canvas size corresponding to the display interface, T Max Indicates the maximum preset amplitude, T R represents the initial relative amplitude corresponding to the simulated aircraft R.

8. 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 6 is implemented.

9. 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, the simulation method of the airborne radar target warning display system according to any one of claims 1 to 6 is implemented.

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