CN117289625A - Interoperation simulation platform and operation method applied to multiple types of aircraft - Google Patents
Interoperation simulation platform and operation method applied to multiple types of aircraft Download PDFInfo
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Abstract
The invention relates to an interoperation simulation platform and an operation method applied to various types of aircrafts, wherein the simulation platform comprises an operation scheduling management module, a combat scene simulation module, a weapon chain simulation module, a data chain simulation module, an aircraft display control simulation module, a sensor simulation module, a flight simulation module and a data conversion module, wherein each simulation module is used for realizing one function simulation in the flight process, the data conversion module is used for generating a data conversion protocol and converting a data format, the operation scheduling management module is used for controlling each simulation module, managing the aircraft model and configuring a data conversion instruction, each simulation module is used for creating the aircraft model and the aircraft instance according to the data conversion instruction, and in the simulation process, format conversion is carried out on service data between each simulation module according to the data conversion protocol to obtain a data format which can be identified by the simulation module, and operation simulation of at least one aircraft model and at least one aircraft instance is carried out. And realizing the interoperation simulation of the multi-model aircraft.
Description
Technical Field
The invention relates to the technical field of airplane operation simulation, in particular to an interoperation simulation platform and an operation method applied to various types of airplanes.
Background
During the flight of an aircraft, various interactive operations are required. Such as the course of the flight, control of the altitude of the flight, acquisition of information such as weather, airports, etc. through a data link, detection of target information on the course by radar, etc. For fighter aircraft, there is also control of weapons, interaction with other fighter aircraft in formation, etc. Therefore, simulation of individual operations of a fighter plane is required to include at least simulation of flight control, simulation of data acquired through a data link, simulation of operation control of sensors, simulation of weapon operations, and simulation of interactions with actual combat scenarios.
In practical application, because the development stages of different types of aircrafts are different, the interface control files (Interface Control Document, abbreviated as ICD) used by the aircrafts are also different, so the following defects exist when the simulation test is performed:
(1) It is necessary to customize its own simulation unit for each model of aircraft. If the aircraft is of the type A and the type B, two flight simulation units are needed to be manufactured to simulate the flight data of the aircraft of the two types respectively.
(2) It is impossible to introduce various types of aircraft in one operational scenario. Because of the data interface differences between different types of aircraft, data communication between the two types of aircraft is not good. This results in instructions on the battlefield not being smoothly delivered to the individual fighter aircraft.
(3) The maintainability and expansibility are poor. When it is desired to modify an aircraft of a certain model or to introduce a new model, it is necessary to introduce all the relevant simulation units, while it is necessary to modify the existing individual simulation units in order to incorporate the identification of the new model aircraft. The maintenance cost is high, and the expansion is inconvenient.
Therefore, how to simulate different types of aircrafts simultaneously to obtain simulation data is a problem to be solved urgently at present.
Disclosure of Invention
The invention aims to provide an interoperation simulation platform and an operation method applied to various types of aircrafts, wherein an operation scheduling management module is arranged in the simulation platform, each simulation module is managed, each aircraft model and each aircraft instance are created, the aircraft model and the aircraft instance identification number and a conversion protocol are configured, each simulation module creates the aircraft model and the aircraft instance under the same identification number according to the instruction of the operation scheduling management module, data format conversion is carried out according to the conversion protocol, a simulation program set with the same function is arranged in each simulation module, a plurality of aircraft instances can be operated when the same simulation program operates, service data and execution actions of each aircraft instance are independent, and interoperation simulation of each aircraft instance is realized.
In a first aspect, the above object of the present invention is achieved by the following technical solutions:
the utility model provides an interoperation simulation platform for multiple model aircraft, including operation dispatch management module, the scene of operation simulation module, weapon chain simulation module, the data chain simulation module, aircraft display control simulation module, sensor simulation module, flight simulation module and data conversion module, each simulation module is used for realizing a function simulation in the flight process, data conversion module is used for generating data conversion protocol and conversion data format, operation dispatch management module is used for controlling each simulation module, manage the aircraft model, configuration data conversion instruction, each simulation module is according to data conversion instruction, establish aircraft model and aircraft instance, in the simulation process, carry out the format conversion to the business data between each simulation module according to data conversion protocol, obtain the data format that can discern by oneself, carry out the operation simulation of at least one aircraft model and at least one aircraft instance.
The invention is further provided with: the data conversion modules are arranged in the operation scheduling management module and each simulation module in a scattered manner, the data conversion modules arranged in the operation scheduling management module in a scattered manner are used for configuring a data conversion protocol for each simulation module according to a user instruction to generate a data conversion instruction of each simulation module, and the data conversion modules arranged in the simulation modules in a scattered manner are used for respectively carrying out format conversion on service data when the simulation modules interact in the simulation process.
The invention is further provided with: at least one simulation program with the same simulation function is integrated in one simulation module, one simulation program is used for executing a specific simulation process, and one simulation program can operate at least one aircraft instance in the simulation process, each aircraft instance has own service data and execution actions, and behaviors among the aircraft instances are not interfered with each other.
The invention is further provided with: the flight simulation module is used for realizing the relevant simulation processing of flight operation; the sensor simulation module comprises a sensor equipment simulation unit, and the sensor equipment simulation unit is used for sending simulation data generated by the sensor to the combat scene simulation module and the aircraft display control simulation module; the weapon chain simulation module comprises a weapon chain management unit, wherein the weapon chain management unit is used for sending the received operation instruction to an aircraft instance or platform with command authority for processing; the aircraft display control simulation module comprises at least one display control unit, and performs relevant flight control operation and display flight parameters on a display control interface of each display control unit, and sends aircraft display control instructions to the weapon chain simulation module, the data chain simulation module and the sensor simulation module; the data link simulation module comprises a data link management unit, and the data link management unit is used for sending an operation instruction to the aircraft display control module and the combat scene simulation module; the fight scene simulation module receives the data of the weapon link management unit, the data link management unit, the sensor simulation unit and the flight simulation module, converts the data into data irrelevant to the model of the aircraft, simulates various models of virtual aircraft, and carries out the collaborative fight simulation of the multiple models of aircraft.
In a second aspect, the above object of the present invention is achieved by the following technical solutions:
the operation method is applied to interoperation simulation platforms of various types of aircrafts, and comprises the steps of running a scheduling management module, sending a management heartbeat frame to each simulation module in a broadcasting mode, receiving the simulation heartbeat frame of each simulation module, acquiring the state information of each simulation module, and broadcasting the state information of each simulation module to all simulation modules through the management heartbeat frame; the method comprises the steps of creating an airplane model and an airplane instance, configuring identification numbers for the airplane model and the airplane instance, managing each simulation module, and deleting the existing airplane model and the existing airplane instance.
The invention is further provided with: the management heartbeat frame comprises a time stamp, an IP address, a port number, a heartbeat time interval and state information of each simulation module, and each simulation heartbeat frame comprises the state information of the simulation module.
The invention is further provided with: the operation of the operation scheduling control module comprises the following steps:
b1, starting;
b2, sending a heartbeat frame to each simulation module;
b3, receiving heartbeat frames of the simulation modules, and determining whether the simulation modules are online;
b4, creating each new model and corresponding airplane instance, respectively configuring an identification number and a data conversion instruction for each model, and sending the identification number, the new model creation instruction and the data conversion instruction to each simulation module on line;
And B5, receiving state information of each simulation module and the creation results of each model of airplane and airplane instance.
In a third aspect, the above object of the present invention is achieved by the following technical solutions:
the operation method applied to the interoperation simulation platform of the airplane with various models comprises a data conversion module and a second data conversion module, wherein the first data conversion module is arranged in an operation scheduling control module and is used for providing a configuration interface of a data conversion protocol, configuring the data conversion protocol and generating a data conversion instruction, and the operation method comprises the following steps:
s1, selecting a simulation module;
s2, selecting corresponding ICD data bits for the fields of each data structure in the selected simulation module.
S3, generating a data conversion instruction for each data structure in the selected simulation module according to the data conversion protocol.
The invention is further provided with: in each simulation module, a second data conversion module is respectively set, and the second data conversion module is used for converting the data received by each simulation module into a data format which can be identified by the second data conversion module according to a conversion protocol, obtaining the corresponding relation between the fields of each interface control file in each simulation module, and establishing a conversion relation table, and the method comprises the following steps:
A1, receiving data;
a2, extracting an identification number in the data;
a3, judging whether a conversion instruction exists in the data, if so, entering the next step, and if not, turning to A2;
a4, analyzing the conversion instruction to obtain an analyzed conversion instruction and a conversion relation table;
a5, extracting a source data position and a target data position in the converted instruction after analysis, wherein the source data represents data to be converted, and the target data represents the converted data;
a6, intercepting specified data content from the received source data according to a conversion protocol;
a7, placing the intercepted data to the position of the target data;
a8, judging whether all the conversions are completed, if yes, converting to A2, and if no, converting to A5.
In a fourth aspect, the above object of the present invention is achieved by the following technical solutions:
the operation method of the interoperation simulation platform applied to the airplanes of various types is characterized in that the operation of a flight simulation module is the premise of other simulation, the method comprises two parts of starting preparation and collaborative simulation, in the starting preparation, the airplane types and airplane examples with corresponding identification numbers are created according to the instruction of an operation management control module, the flight simulation of each airplane example is respectively carried out, simulation generation data are sent to a sensor simulation module, and the control simulation module and a combat scene simulation module are displayed.
In a fifth aspect, the above object of the present invention is achieved by the following technical means:
the operation method of the interoperation simulation platform applied to the airplanes of various models comprises the following steps of:
g1, creating various aircraft instances with the same identification number according to an instruction of an operation management control module, and drawing each aircraft instance on a combat scene map;
g2, receiving service data of each aircraft instance sent by the flight simulation module, and obtaining a data format which can be identified by the aircraft after performing data format conversion;
and G3, controlling each simulated aircraft instance to perform corresponding flight operation on the combat scene map.
In a sixth aspect, the above object of the present invention is achieved by the following technical means:
the operation method of the interoperation simulation platform applied to the airplanes of various models comprises the following steps of starting preparation work and collaborative simulation, wherein the starting preparation work comprises the following steps:
h1, creating various aircraft instances with the same identification number according to the instruction of the operation management control module;
H2, receiving service data of each aircraft instance sent by the flight simulation module, and obtaining a data format which can be identified by the aircraft after performing data format conversion;
and H3, performing sensor simulation operation.
In a seventh aspect, the above object of the present invention is achieved by the following technical means:
the operation method of the interoperation simulation platform applied to the airplanes of various models displays and controls the work of the simulation module, comprising two parts of starting preparation work and collaborative simulation, wherein the starting preparation work comprises the following steps:
r1, creating various types of aircraft examples according to the instruction of the operation management control module and the identification number of the corresponding operation management control module;
r2, after converting the data format according to the conversion protocol, obtaining the data format which can be identified by the user, converting the received data of each aircraft instance sent by the flight simulation module into respective display control data, and transmitting the display control data to each aircraft instance.
In an eighth aspect, the above object of the present invention is achieved by the following technical means:
an operation method of an interoperation simulation platform applied to multiple types of aircrafts, a collaborative simulation process of each simulation module, comprises the following steps:
K1, in the sensor simulation module, an aircraft model radar module finds a target and sends ICD_C_T to the aircraft model display control and combat scene simulation module in the display control simulation module;
k2, the aircraft model display control sends the aircraft model radar data to the display control of the other aircraft models according to the target category; the combat scene simulation module draws a found target on a scene map;
k3, after the display control of the other aircraft models is converted into the radar data which can be identified by the aircraft model through a data conversion module, judging that the attack needs to be initiated, and sending the command control data of the aircraft model to a data chain simulation module so as to request the attack;
k4, after receiving each command control data, the data chain simulation module converts the command control data into own data chain command control data, and then sends the data chain command control data to display and control of the other aircraft models so as to answer the display and control requests of the other aircraft models;
after receiving the response of the data chain simulation module, the display control of the other aircraft models sends own sensor data to the weapon chain simulation module to represent a transmitting weapon;
k6, after receiving the sensor simulation data of each aircraft model, the weapon chain simulation module converts the sensor simulation data into own weapon chain sensor data, performs corresponding weapon emission treatment, and simultaneously sends the weapon chain sensor data to the combat scene simulation module;
And K7, after the combat scene simulation module receives the weapon chain sensor data, simulating weapon emission and striking processes on the combat scene ground.
The above object of the present invention is achieved according to a ninth aspect by:
the interoperation simulation platform terminal comprises a memory, a processor and a computer program which is stored in the memory and can run on the processor, wherein the processor is provided with the computer program and the simulation platform operation program which can realize a simulation platform, and the processor realizes the method when executing the computer simulation platform operation program.
Compared with the prior art, the beneficial technical effects of this application are:
1. according to the method and the device, the operation scheduling management module is arranged to manage each simulation module, so that interactive management of each simulation module is realized;
2. further, the data conversion module is arranged, the conversion protocol is configured, the data conversion instruction is generated, the data format of each simulation module which is independent of each other is converted, interaction among the simulation modules is realized, the data difference of each simulation module is shielded, each simulation module can support the control operation of various types of aircrafts, and simulation data are provided for each type of aircrafts;
3. Further, in the operation scheduling management module and each simulation module, the aircraft model and the aircraft instance with the same identification number are created, so that each data corresponds to each data when the platform is simulated, and the action consistency of the aircraft instance in each simulation module is ensured;
4. furthermore, the interactive operation simulation of the multiple aircraft instances of each simulation unit improves the test efficiency of the interoperation, simplifies the coupling between each simulation unit and the aircraft model, and improves the uniformity, the expandability and the maintainability.
Drawings
FIG. 1 is a schematic diagram of a simulation platform architecture according to an embodiment of the present application;
FIG. 2 is a schematic diagram of a status information structure of each simulation module according to an embodiment of the present application;
FIG. 3 is a schematic diagram of a simulated data processing structure in accordance with one embodiment of the present application;
fig. 4 is a schematic diagram of a conversion flow of the second data conversion module according to an embodiment of the present application.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The interoperation simulation platform is applied to multiple types of aircraft. As shown in FIG. 1, the system comprises an operation scheduling management module, a combat scene simulation module, a weapon chain simulation module, a data chain simulation module, an aircraft display control simulation module, a sensor simulation module, a flight simulation module and a data conversion module, wherein each simulation module operates independently.
The operation scheduling management module is respectively connected with the combat scene simulation module, the weapon chain simulation module, the data chain simulation module, the airplane display control simulation module, the sensor simulation module and the flight simulation module.
The operation scheduling management module is used for generating a data conversion protocol, controlling each simulation module, managing the model of the airplane and configuring data conversion instructions.
Each simulation module refers to one of a combat scene simulation module, a weapon chain simulation module, a data chain simulation module, an aircraft display control simulation module, a sensor simulation module and a flight simulation module.
Each simulation module is used for realizing a simulation function.
The operation scheduling management module comprises a data conversion module 1, and the data conversion module 1 is used for generating a data conversion protocol.
The aircraft display control simulation module comprises a data conversion module 2 and at least one display control unit, wherein in principle, one display control unit is correspondingly arranged for one aircraft model, and the data conversion module 2 is connected with the display control unit.
The data chain simulation module comprises a data conversion module 3 and a data link management unit which are connected in sequence.
The weapon chain simulation module comprises a data conversion module 4 and a weapon chain management unit which are connected in sequence.
The sensor simulation module comprises a data conversion module 5 and a sensor unit which are connected in sequence.
The combat scene simulation module comprises a data conversion module 6.
In order to accurately simulate the structure of the platform, a data conversion module is arranged in each simulation module and used for converting the business data format among the simulation modules and converting the received business data format into a data format which can be identified by the user.
In another embodiment of the present application, the data conversion module is an integral unit, and is disposed in the platform, and each simulation module requests the data conversion module to perform data conversion when needed. In the following description, the data conversion modules are respectively set in each simulation module, and the data conversion modules are collected together for the condition that each simulation module is called, and the like, and are not repeated.
At least one simulation program with the same simulation function is integrated in each simulation module, one simulation program is used for executing a specific simulation process, and one simulation program can operate at least one aircraft instance in the simulation process, each aircraft instance has own service data and execution actions, and the behaviors of the aircraft instances are not interfered with each other.
And (3) an operation scheduling management module:
and sending operation scheduling control instructions to each simulation module, wherein the operation scheduling control instructions comprise operation or stop instructions of each simulation module and airplane model instructions added or deleted.
After each simulation module is online, the system enters a standby state, and the operation scheduling management module sends an operation or stop instruction to each online simulation module to control the operation or stop of each simulation module.
After the operation scheduling management module is online, periodically sending a management heartbeat frame to each simulation module in a broadcast mode, wherein the management heartbeat frame comprises the state information of each simulation module, receiving the simulation heartbeat frame of each simulation module, acquiring the state information of each simulation module from the heartbeat frame of each simulation module, and broadcasting the state information of each simulation module to all simulation modules.
The management heartbeat frame comprises a time stamp, an IP address, a port number, a heartbeat time interval, state information of each simulation module and a check code.
The time stamp is used for time synchronization among the simulation modules.
The IP address and port number are used to run the schedule management module to receive the data.
The status information of each simulation module is configured in a set order, and in a specific embodiment of the present application, as shown in fig. 2, the status information of each simulation module is set in the order: the system comprises a flight simulation unit state, a sensor simulation unit state, a data chain simulation unit state, a weapon chain simulation unit state and a combat scene simulation unit state.
In the operation scheduling management module, a new aircraft model is created, a unique identification number is allocated to the new aircraft model, at least one aircraft instance is created corresponding to the new aircraft model, and the unique identification number is also configured for each aircraft instance.
The data conversion module 1 is used for providing a configuration interface of a data conversion protocol, the user configures the conversion protocol by himself, and a data conversion instruction corresponding to a new aircraft model is generated according to the user conversion protocol.
The operation scheduling management module sends an instruction for creating a new aircraft model and an instruction for creating an aircraft instance to each simulation module, stores the data conversion instruction and the conversion protocol, and each simulation module requests the operation scheduling management module for the data conversion instruction and the conversion protocol when needed.
In one embodiment of the present application, data conversion instructions and conversion protocols are sent to each simulation module, which invokes the data conversion instructions and conversion protocols as needed.
And deleting the existing aircraft model and related data in the operation scheduling management module.
The data conversion module is used for converting the data format of the sender into the data format which can be identified by the receiver according to the conversion protocol.
The functions of each simulation module include: receiving a management heartbeat frame of an operation scheduling management module, acquiring state information of each simulation module, transmitting a simulation heartbeat frame of the simulation module, and reporting a self state; and receiving an instruction for creating the new model number of the airplane and the instance of the airplane by the operation scheduling management module, and creating the model number of the airplane and the instance of the airplane under the corresponding identification number according to the instruction.
The data processing process of each simulation module, as shown in fig. 3, includes: receiving an instruction of creating an aircraft instance by the operation scheduling management module, creating the aircraft instance according to the instruction, generating a data conversion module, converting the service data received by the data conversion module to obtain a data format which can be identified by the data conversion module, and combining specific simulation logic in the simulation module to apply the simulation module to the aircraft instance to generate simulation data.
And the flight simulation module is used for realizing the relevant simulation processing of the flight operation.
After the aircraft model and the aircraft instance under the corresponding identification numbers are created, a flight simulation interface is set for the aircraft model of each identification number, and the flight mode and the flight parameters are configured in the flight simulation interface.
The flight modes include automatic flight, waypoint flight and manual flight, wherein the automatic flight and waypoint flight are based on provided heading, flap, pitch parameters or waypoint data. The manual flight is to connect an aircraft control rocker for manual control flight.
In the simulation process, the flight simulation module runs a flight simulation program, simulation flight of at least one aircraft instance is carried out in the flight simulation program, and flight simulation data generated by flight operation are respectively sent to the sensor simulation module, the flight display control module and the combat scene simulation module.
An aircraft display control simulation module:
comprising a data conversion module 2 and display control units.
After the aircraft model and the aircraft instance under the corresponding identification numbers are created, a display control interface corresponding to the identification numbers is created for each aircraft model, each display control interface is integrated in an aircraft display control simulation module in a modular mode, and the display interfaces and the internal data processing of each display control unit are completely independent and mutually independent.
In the simulation process, the same calling mode is adopted to call each aircraft display control simulation program, and when a new aircraft model and an aircraft instance exist, the display control components of the aircraft instance of the model can be dynamically integrated. And simulating a display control interface on the aircraft in the display control unit, performing relevant flight control operation and display flight parameters on the display control interface, and sending aircraft display control instructions to the weapon chain simulation module, the data chain simulation module and the sensor simulation module, wherein the aircraft display control instructions comprise aircraft operation parameter instructions.
The data conversion module in the aircraft display control module converts the received service data format in each simulation module, displays related data, dynamically displays current flight parameters of the aircraft on a display interface after receiving the flight data sent by the flight simulation module, comprises information such as current height, heading, pitching angle and the like of the aircraft, and displays a target position on a radar interface of the display control unit when receiving target data sent by the sensor simulation module.
And inputting a control instruction on the aircraft display control interface, and after receiving the control instruction, the aircraft display control module sends the control instruction to a corresponding simulation program and receives data information fed back by the corresponding simulation program.
If the control instruction is to display the scanning range of the radar, the aircraft display control module sends the control instruction to the sensor simulation module, the sensor simulation module transmits the current radar scanning range data of the aircraft instance to the aircraft display control module, and after the data conversion module converts the radar scanning range data, the aircraft display control module displays the radar scanning range on a display interface.
If the control instruction is to check airport information, the aircraft display control module sends the control instruction to the data chain simulation module, the data conversion module in the data chain simulation module converts the received data, the converted data can be recognized by the data chain simulation module, the corresponding airport data is sent to the aircraft display control module according to the converted data, and the aircraft display control unit also obtains a data format which can be recognized by the aircraft display control unit through the conversion of the data conversion module and displays the data.
Sensor simulation module:
comprising a data conversion module 5 and a sensor device emulation unit.
After the aircraft model and the aircraft instance under the corresponding identification numbers are created, the aircraft data sent by the flight simulation module are received for the aircraft model under each identification number, and the data conversion module 5 converts the aircraft data into a data format which can be recognized by the aircraft data, so that the functional simulation of various sensor devices is performed.
Sensor devices include fire radars, photoelectric radars, and electronic warfare.
The sensor equipment simulation unit sends simulation data generated by the sensor to the combat scene simulation module and the aircraft display control simulation module.
Weapon chain simulation module:
the method is used for weapon coordination and combat coordination simulation among aircraft instances in formation. Comprising a weapon link management unit and a data conversion module 4.
After the aircraft model and the aircraft instance under the same identification number are created, in the simulation process, the data conversion module 4 converts the request data sent by the aircraft display control module into an operation instruction which can be identified by the data conversion module, and according to the operation instruction, the weapon link management unit generates related data or forwards the operation instruction to other related aircraft instances in the simulation process.
For example, after receiving the attack request instruction sent by the aircraft display control module, the weapon chain simulation module obtains an operation instruction after conversion by the data conversion module 4, and the weapon chain management unit sends the operation instruction to an aircraft instance or platform with command authority for processing.
And the data and the instructions generated by the weapon chain simulation module are transmitted to the combat scene simulation module, and are used for realizing the collaborative simulation of the combat unit and the command unit in the combat scene.
And the data chain simulation module:
comprising a data link management unit and a data conversion module 3.
After the aircraft model and the aircraft instance under the same identification number are created, in the simulation process, request data sent by the aircraft display control are received, an operation instruction capable of identifying a data format is obtained through conversion of the data conversion module 3, relevant data are generated according to the operation instruction, and the data link management unit sends the generated data to the aircraft display control module and the combat scene simulation module.
The data chain simulation module is used for simulating flight related data on an aircraft example, including meteorological data, airport data and literature and electricity information.
The combat scene simulation module:
the simulation system is used for simulating a battlefield environment, and under the battlefield environment, the online simulation module data are fused to realize the simulation of the whole battlefield condition.
In the simulation process, the fight scene simulation module receives data of the weapon link management unit, the data link management unit, the sensor simulation unit and the flight simulation module, and obtains data format instructions which can be recognized by the fight scene simulation module through conversion of the data conversion module 6, wherein the converted data are irrelevant to the model of each aircraft, virtual aircrafts of various models are simulated according to the converted data in the fight scene, the fight scene simulation is carried out on the multiple models of aircrafts, each virtual aircrafts is a fight unit, and a fight command control center is simulated according to each command data to serve as a command unit.
The combat scene simulation module is combined with OSG (OpenSceneGraphic) technology to simulate the environment of a real combat scene, and draw the flight process, radar scanning action, weapon attack action and the like. Among these, OSG technology is a high-level graphics development interface based on industry graphics standards.
The inside of each simulation module comprises service data, the service data of each simulation module is only relevant to respective service, when a certain model of airplane needs to adopt the service data in each simulation module or a certain model of flight operation instruction is sent to each simulation module for processing, the data is subjected to format conversion by adopting a data conversion module according to a data conversion protocol and a conversion instruction configured when a new model is added.
When the operation scheduling control module creates a new model of airplane, configuring related conversion instructions, sending the new model of airplane creation instructions and the conversion instructions to each simulation module, after receiving the corresponding instructions of the operation scheduling control module, each simulation module creates corresponding conversion models according to respective data formats, and when each simulation module receives data, data conversion is carried out by using the respective conversion models.
The operation scheduling control module and each simulation module respectively comprise a data conversion module.
And operating a first data conversion module in the scheduling control module, providing a configuration interface of a data conversion protocol, configuring the data conversion protocol, and generating a data conversion instruction.
The method comprises the following steps:
s1, selecting a simulation module;
s2, selecting corresponding ICD data bits for the fields of each data structure in the selected simulation module.
S3, generating a data conversion instruction for each data structure in the selected simulation module according to the data conversion protocol.
The data conversion instruction resembles an array, as shown in the following:
114126156223
the 1 st digit in each group represents the identification number of the data structure in the selected simulation module, the 2 nd digit represents the start byte of the field in the data structure, the 3 rd digit represents the end byte of the field in the data structure, the 4 th digit represents the ICD (Interface Control Document interface control file) identification number of the new model, the 5 th digit represents the start byte in the ICD identification number, and the 6 th digit represents the end byte in the ICD identification number.
A simulation module includes at least one data structure, and when a new aircraft model is added, a respective data conversion instruction is correspondingly created for each data structure.
Each simulation module comprises a second data conversion module, the second data conversion module in each simulation module provides a data conversion analysis instruction, and the function of generating a data conversion model is achieved according to the data interface definition of each simulation unit. For simplicity of starting point, each simulation module is simply referred to as a simulation module, and only refers to one simulation module correspondingly, but not to a collective term of all simulation modules, the second data conversion module is one of the data conversion modules 2-6, and the second data conversion module converts when there is data conversion, and is in a standby state when there is no data to be converted.
After receiving the data conversion instruction, the simulation module calls a second data conversion module in the simulation module, analyzes the data conversion instruction and generates a data conversion model used by the simulation module according to the requirement.
The second data conversion in each simulation module, as shown in fig. 4, the operation process includes the following steps:
a1, receiving data;
a2, extracting an identification number in the data;
a3, judging whether a conversion instruction exists in the data, if so, entering the next step, and if not, turning to A2;
a4, analyzing the conversion instruction to obtain an analyzed conversion instruction and a conversion relation table;
A5, extracting a source data position and a target data position in the converted instruction after analysis, wherein the source data represents data to be converted, and the target data represents the converted data;
a6, intercepting specified data content from the received source data according to a conversion protocol;
a7, placing the intercepted data to the position of the target data;
a8, judging whether all the conversions are completed, if yes, converting to A2, and if no, converting to A5.
And obtaining the corresponding relation among the ICD fields in each simulation module according to the analyzed conversion instruction, and establishing a conversion relation table.
For the purpose of simplifying the starting point for description, the method for operating the interoperation simulation platform applied to the airplanes of various types uses two types of airplanes as an illustration of a joint simulation process, and the like, the case of joint simulation of more than two types of airplanes is omitted.
In the process of creating a new model aircraft model, the operation of the operation scheduling control module comprises the following steps:
b1, starting;
b2, sending a heartbeat frame to each simulation module;
b3, receiving heartbeat frames of the simulation modules, and determining whether the simulation modules are online;
the method comprises the steps of B4, creating two new types of aircrafts, configuring identification numbers of the new types of aircrafts, respectively configuring a first model and a second model, configuring a first data conversion instruction for the first model, configuring a second data conversion instruction for the second model, and sending the identification numbers, the new type creation instruction and the data conversion instruction to each online simulation module;
And B5, receiving state information of each simulation module and the creation result of each model of airplane model.
The operation of each simulation module comprises the following steps:
c1, starting;
c2, receiving a heartbeat frame of the operation scheduling control module, and acquiring state information of all online simulation modules;
c3, receiving a new model creation instruction and a data conversion instruction of the operation scheduling control module,
c4, creating a new model airplane model;
c5, for each new model number of aircraft, creating at least one aircraft instance;
in one embodiment of the present application, a cooperative combat simulation of a drone and helicopter is illustrated. And the same is true for the collaborative combat simulation of a plurality of models, and the description is omitted.
Setting identification numbers for each type of aircraft:
the ICD file of the unmanned plane is expressed as ICD_A, the ICD file of the helicopter is expressed as ICD_B, and the ICD file used by the simulation module itself is expressed as ICD_C.
Marking service data and applied simulation modules of each model of airplane:
service data of the unmanned aerial vehicle, including aircraft data and radar data, are respectively expressed as follows:
ICD_A_F, which is flight data applied to a display control simulation module, a sensor simulation module and a combat scene simulation module;
Icd_a_t: radar data applied to a display control simulation module and a combat scene simulation module;
the service data of the helicopter comprise aircraft data, radar data, fire control data and command control data, and are respectively expressed as follows:
ICD_B_F, which is applied to a display control simulation module, a sensor simulation module and a combat scene simulation module;
icd_b_t: radar data applied to a display control simulation module and a combat scene simulation module;
icd_b_w: fire control data applied to a weapon chain simulation module and a combat scene simulation module;
icd_b_c: and commanding and controlling data, which is applied to the data chain simulation module and the combat scene simulation module.
Marking service data of the aircraft in different simulation modules:
the flight simulation module internal data, including flight data, is represented as follows:
icd_c_f: flight data.
The sensor simulation module internal data comprises aircraft data and radar data, and the data are respectively expressed as follows:
icd_c_f: flight data, the same as the representation of the flight simulation module;
icd_c_t: radar data.
The weapon chain simulation module internal data, including fire control data, is represented as follows:
icd_c_w: fire control data.
The data chain simulation module internal data, including command control data, is expressed as follows:
Icd_c_c: command control data.
The internal data of the combat scene simulation module, including aircraft data, radar data and fire control data, are respectively represented as follows:
ICD_C_F, the flight data is the same as the representation of the flight simulation module;
ICD_C_T, radar data;
ICD_C_W fire control data, the same as the representation in the weapon chain simulation module.
After the simulation platform is started, the work of each module comprises two steps of starting preparation and simulation cooperation, and the two steps are respectively described.
D1, starting preparation;
the starting preparation work of the operation scheduling management module comprises the following steps:
e1, creating two models of the unmanned plane and the helicopter, and importing all ICD identification numbers under the two models.
E2, configuring data conversion protocols of each simulation module of the unmanned plane and the helicopter;
in different simulation modules, the conversion relationship is as follows:
and a display control simulation module:
unmanned aerial vehicle: ICD_C_F- > ICD_A_ F, ICD _C_T- > ICD_A_T, namely converting the simulated flight data format into the unmanned aerial vehicle flight data format, and converting the simulated radar data format into the unmanned aerial vehicle radar data format;
helicopter: icd_c_f- > icd_b_ F, ICD _c_t- > icd_b_ T, ICD _a_t- > icd_b_t, i.e., converting the simulated flight data format to a helicopter flight data format, converting the simulated radar data format to a helicopter radar data format, and converting the unmanned plane radar data format to a helicopter radar data format;
And the data chain simulation module:
ICD_B_C- > ICD_C_ C, ICD _C- > ICD_B_C, namely converting the helicopter command control data format into a simulation command control data format, and converting the simulation command control data format into the helicopter command control data format.
Weapon chain simulation module:
helicopter: ICD_B_W- > ICD_C_W converts the helicopter fire control data format to a simulated fire control data format.
E3, creating an airplane example F1 for the unmanned plane model number and creating an airplane example Z1 for the helicopter model number;
and E4, sending an instruction for creating the unmanned aerial vehicle, the helicopter and the airplane instance to each simulation module.
The flight simulation is the premise of other simulation, and the starting preparation work of the flight simulation module comprises the following steps:
f1, a flight simulation module creates an instance of an unmanned plane and a helicopter corresponding to the identification numbers according to the instruction of the management module, and the instances are named as F1 and Z1;
f2, respectively performing flight simulation of F1 and Z1, and then sending ICD_C_F data of F1 and ICD_C_F data of Z1 to the sensor simulation module, the display control simulation module and the combat scene simulation module.
The operation scene simulation module starts preparation work, which comprises the following steps:
g1, creating an instance of the unmanned aerial vehicle and a helicopter, which are named as F1 and Z1, according to the instruction of the operation management control module and corresponding to the identification number of the operation management control module; drawing an unmanned plane and a helicopter on a combat scene map;
G2, receiving ICD_C_F of F1 and ICD_C_F of Z1 sent by a flight simulation module, and obtaining a data format which can be identified by the user after performing data format conversion;
and G3, controlling the unmanned aerial vehicle and the helicopter which are drawn out by the model on the combat scene map to carry out corresponding flight operation processing.
The method for preparing the sensor simulation module for starting comprises the following steps:
h1, according to the instruction of the operation management control module, an instance of an unmanned aerial vehicle and a helicopter is created corresponding to the identification number of the operation management control module, and the instance is named as F1 and Z1;
h2, receiving ICD_C_F of F1 and ICD_C_F of Z1 sent by the flight simulation module, and obtaining a data format which can be identified by the user after performing data format conversion;
and H3, performing simulation operation, including radar scanning simulation, fire control simulation and the like.
The display control simulation module starts preparation work, which comprises the following steps:
r1, according to the instruction of the operation management control module, creating an instance of an unmanned aerial vehicle and a helicopter, which are named as F1 and Z1, corresponding to the identification number of the operation management control module;
r2, converting the data format according to a conversion protocol to obtain a data format which can be identified by the data format, converting the received ICD_C_F data of the F1 sent by the flight simulation module into ICD_A_F data of the unmanned aerial vehicle, and transmitting the ICD_A_F data to display control of the F1; and converting the received ICD_C_F data of the Z1 sent by the flight simulation module into ICD_B_F data of the helicopter, and transmitting the ICD_C_F data to display control of the Z1.
D2, collaborative combat simulation process:
k1, in the sensor simulation module, the radar module of the unmanned aerial vehicle finds a target and sends ICD_C_T to the F1 display control and combat scene simulation module in the display control simulation module;
k2, F1 display control sends ICD_A_T to Z1 display control according to the target category; the combat scene simulation module draws a found target on a scene map;
k3, Z1 display control converts ICD_A_T into ICD_B_T through a data conversion module, determines that attack needs to be initiated, and sends ICD_B_C to a data chain simulation module to request attack;
k4, the data chain simulation module receives the ICD_B_C and converts the ICD_C_C into ICD_C_C, and then transmits the ICD_C_C to the Z1 display control to answer the Z1 display control request;
after receiving the response of the data chain simulation module, the display controller K5 and the display controller Z1 send ICD_B_W to the weapon chain simulation module to represent a transmitting weapon;
k6, after receiving ICD_B_W, the weapon chain simulation module converts the ICD_B_W into ICD_C_W, performs corresponding weapon emission treatment, and simultaneously sends ICD_C_W to the combat scene simulation module;
and K7, after the combat scene simulation module receives the ICD_C_W, simulating weapon firing and striking processes on the combat scene ground.
Thus, the collaborative combat simulation of the unmanned plane and the helicopter is completed.
An embodiment of the present invention provides a terminal device of an interoperable simulation platform applied to multiple types of aircraft, where the terminal device of the embodiment includes: a processor, a memory, and computer programs stored in the memory and executable on the processor, such as simulation platform programs and simulation platform operating programs, which when executed implement the methods described herein.
The computer program may be divided into one or more modules/units, which are stored in the memory and executed by the processor to accomplish the present invention, for example. The one or more modules/units may be a series of computer program instruction segments capable of performing specific functions for describing the execution of the computer program in the terminal device of the interoperable simulation platform for use in a plurality of types of aircraft. For example, the computer program may be divided into a plurality of modules, each module having a specific function as described herein.
The interoperation simulation platform terminal equipment applied to the airplanes with various models can be computing equipment such as desktop computers, notebooks, palm computers and cloud servers. The terminal equipment of the interoperation simulation platform applied to the airplane with various models can comprise, but is not limited to, a processor and a memory. It will be appreciated by those skilled in the art that the above examples are merely examples of the interoperable simulation platform terminal device applied to multiple models of aircraft, and are not limiting of the interoperable simulation platform terminal device applied to multiple models of aircraft, and may include more or fewer components than illustrated, or combine certain components, or different components, e.g., the interoperable simulation platform terminal device applied to multiple models of aircraft may further include input and output devices, network access devices, buses, etc.
The processor may be a central processing unit (Central Processing Unit, CPU), but may also be other general purpose processors, data signal processors (Digital Signal Processor, DSP), application specific integrated circuits (Application Specific Integrated Circuit, ASIC), off-the-shelf programmable gate arrays (Field-Programmable Gate Array, FPGA) or other programmable logic devices, discrete gate or transistor logic devices, discrete hardware components, or the like. The general purpose processor may be a microprocessor or the processor may be any conventional processor or the like, and the processor is a control center of the terminal device of the interoperable simulation platform applied to the multiple types of aircrafts, and the various interfaces and lines are used to connect various parts of the entire terminal device of the interoperable simulation platform applied to the multiple types of aircrafts.
The memory may be used to store the computer program and/or the module, and the processor may implement the various functions of the terminal device of the interoperable simulation platform applied to multiple types of aircraft by running or executing the computer program and/or the module stored in the memory and invoking the data stored in the memory. The memory may mainly include a storage program area and a storage data area, wherein the storage program area may store an operating system, an application program (such as a sound playing function, an image playing function, etc.) required for at least one function, and the like; the storage data area may store data (such as audio data, phonebook, etc.) created according to the use of the handset, etc. In addition, the memory may include high speed random access memory, and may also include non-volatile memory, such as a hard disk, memory, plug-in hard disk, smart Media Card (SMC), secure digital (SecureDigital, SD) Card, flash Card (Flash Card), at least one disk storage device, flash memory device, or other volatile solid state memory device.
The module/unit integrated with the terminal device of the interoperable simulation platform applied to the aircrafts with various models can be stored in a computer readable storage medium if the module/unit is implemented in the form of a software functional unit and sold or used as a separate product. Based on such understanding, the present invention may implement all or part of the flow of the method of the above embodiment, or may be implemented by a computer program to instruct related hardware, where the computer program may be stored in a computer readable storage medium, and when the computer program is executed by a processor, the computer program may implement the steps of each of the method embodiments described above. Wherein the computer program comprises computer program code which may be in source code form, object code form, executable file or some intermediate form etc. The computer readable medium may include: any entity or device capable of carrying the computer program code, a recording medium, a U disk, a removable hard disk, a magnetic disk, an optical disk, a computer memory, a Read-only memory (ROM), a random access memory (RAM, random Access Memory), an electrical carrier signal, a telecommunications signal, a software distribution medium, and so forth.
The above embodiments are not intended to limit the scope of the present invention, so: all equivalent changes in structure, shape and principle of the invention should be covered in the scope of protection of the invention.
Claims (10)
1. The utility model provides an interoperation simulation platform for multiple model aircraft which characterized in that: the system comprises an operation scheduling management module, a combat scene simulation module, a weapon chain simulation module, a data chain simulation module, an aircraft display control simulation module, a sensor simulation module, a flight simulation module and a data conversion module, wherein each simulation module is used for realizing functional simulation in the flight process, the data conversion module is used for generating a data conversion protocol and converting a data format, the operation scheduling management module is used for controlling each simulation module, managing aircraft models and configuring data conversion instructions, each simulation module is used for creating aircraft models and aircraft instances according to the data conversion instructions, and in the simulation process, format conversion is carried out on business data among each simulation module according to the data conversion protocol to obtain a data format which can be identified by the simulation module, and operation simulation of at least one aircraft model and at least one aircraft instance is carried out.
2. An interoperable simulation platform for use with multiple models of aircraft as claimed in claim 1, wherein: the data conversion modules are arranged in the operation scheduling management module and each simulation module in a scattered manner, and are used for configuring a data conversion protocol for each simulation module according to a user instruction, generating a data conversion instruction of each simulation module, and carrying out format conversion on service data when each simulation module interacts in the simulation process;
at least one simulation program with the same simulation function is integrated in one simulation module, one simulation program is used for executing a specific simulation process, and one simulation program can operate at least one aircraft instance in the simulation process, each aircraft instance has own service data and execution actions, and the behaviors among the aircraft instances are not interfered with each other;
the flight simulation module is used for realizing the relevant simulation processing of flight operation; the sensor simulation module comprises a sensor equipment simulation unit, and the sensor equipment simulation unit is used for sending simulation data generated by the sensor to the combat scene simulation module and the aircraft display control simulation module; the weapon chain simulation module comprises a weapon chain management unit, wherein the weapon chain management unit is used for sending the received operation instruction to an aircraft instance or platform with command authority for processing; the aircraft display control simulation module comprises at least one display control unit, and performs relevant flight control operation and display flight parameters on a display control interface of each display control unit, and sends aircraft display control instructions to the weapon chain simulation module, the data chain simulation module and the sensor simulation module; the data link simulation module comprises a data link management unit, and the data link management unit is used for sending an operation instruction to the aircraft display control module and the combat scene simulation module; the fight scene simulation module receives the data of the weapon link management unit, the data link management unit, the sensor simulation unit and the flight simulation module, converts the data into data irrelevant to the model of the aircraft, simulates various models of virtual aircraft, and carries out the collaborative fight simulation of the multiple models of aircraft.
3. An operation method of an interoperation simulation platform applied to multiple types of aircrafts is characterized in that: the operation scheduling management module sends a management heartbeat frame to each simulation module in a broadcasting mode, receives the simulation heartbeat frame of each simulation module, acquires the state information of each simulation module, and broadcasts the state information of each simulation module to all simulation modules through the management heartbeat frame; creating an airplane model and an airplane instance, configuring an identification number for the airplane model and the airplane instance, managing each simulation module, and deleting the existing airplane model and the existing airplane instance;
the management heartbeat frame comprises a time stamp, an IP address, a port number, a heartbeat time interval and state information of each simulation module, and each simulation heartbeat frame comprises the state information of the simulation module.
4. A method of operating an interoperable simulation platform for a plurality of aircraft models as claimed in claim 3, wherein: the operation of the operation scheduling control module comprises the following steps:
b1, starting;
b2, sending a heartbeat frame to each simulation module;
b3, receiving heartbeat frames of the simulation modules, and determining whether the simulation modules are online;
b4, creating each new model and corresponding airplane instance, respectively configuring an identification number and a data conversion instruction for each model, and sending the identification number, the new model creation instruction and the data conversion instruction to each simulation module on line;
And B5, receiving state information of each simulation module and the creation results of each model of airplane and airplane instance.
5. An operation method of an interoperation simulation platform applied to multiple types of aircrafts is characterized in that: the data conversion module comprises a first data conversion module and a second data conversion module, wherein the first data conversion module is arranged in the operation scheduling control module and is used for providing a configuration interface of a data conversion protocol, configuring the data conversion protocol and generating a data conversion instruction, and the data conversion module comprises the following steps:
s1, selecting a simulation module;
s2, selecting corresponding ICD data bits for the fields of each data structure in the selected simulation module;
s3, generating a data conversion instruction for each data structure in the selected simulation module according to the data conversion protocol.
6. The method of operation of an interoperable simulation platform for a plurality of aircraft models according to claim 5, wherein: in each simulation module, a second data conversion module is respectively set, and the second data conversion module is used for converting the data received by each simulation module into a data format which can be identified by the second data conversion module according to a conversion protocol, obtaining the corresponding relation between the fields of each interface control file in each simulation module, and establishing a conversion relation table, and the method comprises the following steps:
A1, receiving data;
a2, extracting an identification number in the data;
a3, judging whether a conversion instruction exists in the data, if so, entering the next step, and if not, turning to A2;
a4, analyzing the conversion instruction to obtain an analyzed conversion instruction and a conversion relation table;
a5, extracting a source data position and a target data position in the converted instruction after analysis, wherein the source data represents data to be converted, and the target data represents the converted data;
a6, intercepting specified data content from the received source data according to a conversion protocol;
a7, placing the intercepted data to the position of the target data;
a8, judging whether all the conversions are completed, if yes, converting to A2, and if no, converting to A5.
7. An operation method of an interoperation simulation platform applied to multiple types of aircrafts is characterized in that: the operation scene simulation module comprises a start preparation work and a collaborative simulation, wherein the start preparation work comprises the following steps:
g1, creating various aircraft instances with the same identification number according to an instruction of an operation management control module, and drawing each aircraft instance on a combat scene map;
g2, receiving service data of each aircraft instance sent by the flight simulation module, and obtaining a data format which can be identified by the aircraft after performing data format conversion;
And G3, controlling each simulated aircraft instance to perform corresponding flight operation on the combat scene map.
8. An operation method of an interoperation simulation platform applied to multiple types of aircrafts is characterized in that: the operation of the sensor simulation module comprises two parts of starting preparation work and collaborative simulation, wherein the starting preparation work comprises the following steps:
h1, creating various aircraft instances with the same identification number according to the instruction of the operation management control module;
h2, receiving service data of each aircraft instance sent by the flight simulation module, and obtaining a data format which can be identified by the aircraft after performing data format conversion;
and H3, performing sensor simulation operation.
9. An operation method of an interoperation simulation platform applied to multiple types of aircrafts is characterized in that: the collaborative simulation process of each simulation module comprises the following steps:
k1, in the sensor simulation module, an aircraft model radar module finds a target and sends ICD_C_T to the aircraft model display control and combat scene simulation module in the display control simulation module;
k2, the aircraft model display control sends the aircraft model radar data to the display control of the other aircraft models according to the target category; the combat scene simulation module draws a found target on a scene map;
K3, after the display control of the other aircraft models is converted into the radar data which can be identified by the aircraft model through a data conversion module, judging that the attack needs to be initiated, and sending the command control data of the aircraft model to a data chain simulation module so as to request the attack;
k4, after receiving each command control data, the data chain simulation module converts the command control data into own data chain command control data, and then sends the data chain command control data to display and control of the other aircraft models so as to answer the display and control requests of the other aircraft models;
after receiving the response of the data chain simulation module, the display control of the other aircraft models sends own sensor data to the weapon chain simulation module to represent a transmitting weapon;
k6, after receiving the sensor simulation data of each aircraft model, the weapon chain simulation module converts the sensor simulation data into own weapon chain sensor data, performs corresponding weapon emission treatment, and simultaneously sends the weapon chain sensor data to the combat scene simulation module;
and K7, after the combat scene simulation module receives the weapon chain sensor data, simulating weapon emission and striking processes on the combat scene ground.
10. An interoperable simulation platform terminal for use with a plurality of aircraft models, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, characterized in that: the processor is provided with a computer program capable of realizing a simulation platform and a simulation platform operation program, and the method according to any one of claims 3-9 is realized when the processor executes the computer simulation platform operation program.
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