CN112308422A - Task planning and solving simulation system and method for remote aerial support carrier - Google Patents
Task planning and solving simulation system and method for remote aerial support carrier Download PDFInfo
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Abstract
The invention provides a mission planning and resolving simulation system and method for a remote aerial support carrier, wherein a battlefield force generation platform is used for battle scene configuration, and enemy and my force motion simulation and simulation process management except the carrier, the mission planning and fire control resolving platform is used for situation threat assessment, mission planning, fire control resolving, carrier air route planning and motion simulation, weapon launching control, efficiency assessment and simulation deduction display, and the battlefield force generation platform is connected with the mission planning and fire control resolving platform through an Ethernet. The invention verifies the remote air support airborne combat process and information interaction; programming development and testing are facilitated, good expandability is achieved, and task planning and resolving algorithms can be effectively verified; the algorithm verification requirements under different battle scenes are flexibly adapted; the battlefield situation in the simulation process is visually displayed, the planning and resolving results of all modules are displayed in an overlapping mode, and a user can conveniently verify the rationality and the correctness of a task planning and resolving algorithm.
Description
Technical Field
The invention relates to the technical field of computer simulation, in particular to a task planning and solving simulation system and method for a remote aerial support carrier.
Background
In air-air countermeasure, the remote air support carrier modified from bombers, airliners and the like carries a large number of missiles, and the long-term air-air missile can be launched from the outside of a defense area, so that the fighter plane of one party is fully supported, and the target formation of the enemy is killed. In order to meet the combat requirements, the remote aerial support aircraft needs to have the functions of task planning and resolving, weapons can be reasonably distributed according to the forces of enemy and my arms, fire control resolving is completed, and an aircraft flight path is planned. When the task planning and resolving algorithm of the remote aerial support carrier is researched, a computer is used for building a simulation system for simulation, so that the battle scene can be set conveniently and quickly, the task planning and resolving result can be displayed visually, the task planning and resolving algorithm can be verified economically and flexibly, and the technical support is provided for the development of the remote aerial support carrier.
However, the existing simulation system and method do not consider the operational characteristics of the remote aerial support carrier, and are not suitable for the operational scene of the remote aerial support carrier; the functional requirements of the remote aerial support carrier for distributing weapons, performing fire control calculation and planning flight paths cannot be met, and the mission planning and calculation algorithm of the remote aerial support carrier cannot be verified quickly.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides a mission planning and solution simulation system and method for a remote aerial support carrier. In order to overcome the defect that the prior art is not suitable for a remote aerial support aerial combat scene and effectively verify the task planning and solving algorithm of the remote aerial support aerial carrier, the invention provides a task planning and solving simulation system and method for the remote aerial support aerial carrier.
The technical scheme adopted by the invention for solving the technical problems is as follows:
a mission planning and resolving simulation system for a remote aerial support carrier comprises a battlefield force generation platform and a mission planning and fire control resolving platform;
the battlefield force generation platform is used for battle scene configuration, enemy and my force movement simulation and simulation process management except for the carrier, the task planning and fire control resolving platform is used for situation threat assessment, task planning, fire control resolving, carrier air route planning and movement simulation, weapon emission control, efficiency assessment and simulation deduction display, and the battlefield force generation platform is connected with the task planning and fire control resolving platform through the Ethernet.
The battlefield force generation platform comprises a battlefield force management module, a database module and a network communication module.
The battlefield force management module reads the battle scene stored in the database, provides an operation interface for configuring parameters of battlefield planning, airborne weapons and simulation entities in the battle scene for a user, provides a simulation deduction process management function, and simulates enemy and my force movement except the airborne weapon. And meanwhile, storing the combat scenes configured by the user into a database module, wherein the specific process comprises the steps of firstly reading the combat scenes (comprising battlefield scenario, airborne weapons and simulation entity parameters) in the database and displaying the combat scenes in an operation interface for the user to modify, after the user modifies the configuration, storing the configured combat scenes into the database module, and sending the combat scenes configured by the user and the force and movement information of the enemy and my arms to a task planning and fire control resolving platform through a network communication module.
The database module provides an interface for accessing and operating the database, and stores the battle scenes configured by the users in a database file.
The network communication module realizes communication between the battlefield force generation platform and the mission planning and fire control resolving platform and sends fighting scene configuration and enemy force movement information in the fighting simulation process.
The mission planning and fire control calculation platform comprises a network communication module, a situation threat assessment module, a mission planning module, a fire control calculation module, an aircraft air route planning and simulation module, a weapon management module, a performance assessment module and a simulation deduction display module.
The network communication module realizes communication between the mission planning and fire control resolving station and the battlefield force generating station, receives battle scene configuration and enemy force movement information in the battle simulation process, and distributes the received information to other modules of the mission planning and fire control resolving station.
The situation threat assessment module calculates situation threats of the targets relative to the aerial carrier and the fighter in the same party respectively according to the force and motion information of the enemy and the my, comprehensively assesses the threat degree of each target in the target formation, and sends situation threat assessment results to the task planning module and the simulation deduction display module.
The task planning module completes fire planning and task allocation according to the configuration of the airborne weapons, weapon parameters and situation threat assessment results in the operational scene, gives a launching mode suggestion, and sends the task planning results to the fire control resolving module, the weapon management module and the simulation deduction display module.
The fire control calculation module calculates weapon attack areas, weapon launching points and weapon waypoints according to the operational scene configuration, the target motion information and the task planning result, and sends the fire control calculation result to the carrier route planning and simulation module, the weapon management module and the simulation deduction display module.
The aircraft route planning and simulation module generates an aircraft route point of the aircraft flying to the weapon launching point according to the aircraft performance parameters and the position of the weapon launching point in the fire control calculation result, simulates the aircraft flying to the weapon launching point, sends the aircraft route planning result to the simulation deduction display module, and sends the aircraft motion information to the weapon management module, the efficiency evaluation module and the simulation deduction display module.
The weapon management module simulates weapon state display and weapon emission control processes, simulates weapon emission parameter binding according to a task planning result, and judges whether the carrier reaches a weapon emission point according to carrier motion information and a fire control resolving result. And after the carrier reaches the weapon launching point, simulating the weapon launching process and sending the weapon launching state to the efficiency evaluation module.
After the weapon is launched, the efficiency evaluation module estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target and the aircraft carrier position during weapon launching, estimates the damage probability of the single target, and sends the efficiency evaluation result to the simulation deduction display module.
The simulation deduction display module displays a two-dimensional battlefield environment and forces of enemy and my arms in the simulation process and displays a task planning and resolving result in the fighting simulation deduction process.
A method for realizing a mission planning and solution simulation system for a remote aerial support carrier comprises the following detailed steps:
step 1: connecting a database;
the battlefield force generation database module completes database file connection initialization, reads the battle scene stored in the database, and enters step 2 after database connection is completed;
step 2: configuring a battle scene and initializing simulation deduction display;
in a battlefield force generation platform, a battlefield force management module displays a battlefield scene stored in a database, a user configures parameters of battlefield planning, airborne weapons and simulation entities in the battlefield, a network communication module sends the configured battlefield scene to a mission planning and fire control resolving platform, and after the mission planning and fire control resolving platform receives the battlefield scene, a simulation deduction display module initializes and displays a battlefield environment and forces of enemy and my, and the step 3 is entered;
and step 3: assessing situation threats;
a situation threat assessment module of the task planning and fire control resolving station calculates situation threats of targets relative to the aerial carrier and the fighter of the party respectively according to the force and motion information of the enemy and considering target performance parameters, comprehensively assesses the threat degree of each target in the target formation to obtain a situation threat assessment result, sends the situation threat assessment result to a task planning module and a simulation deduction display module, displays the situation threat assessment result by the simulation deduction display module, and enters step 4;
and 4, step 4: planning a task;
a task planning module of the task planning and fire control calculation table finishes fire planning and task allocation according to the configuration of airborne weapons, weapon parameters and situation threat assessment results in an operational scene, gives weapons required by different emission frequencies and emission mode suggestions that each emission frequency should adopt simultaneous emission or continuous emission according to the fire planning and task allocation results and by considering emission constraints, finally obtains a task planning result, sends the task planning result to a fire control calculation module, a weapon management module and a simulation deduction display module, and the simulation deduction display module displays the task planning result and enters step 5;
and 5: calculating fire control;
calculating a weapon attack area, a weapon launching point and a weapon waypoint by a fire control calculation module of the mission planning and fire control calculation table according to the operational scene configuration, the target motion information and the mission planning result to obtain a fire control calculation result, sending the fire control calculation result to a carrier route planning and simulation module, a weapon management module and a simulation deduction display module, displaying the fire control calculation result by the simulation deduction display module, and entering the step 6;
step 6: planning an aircraft route and simulating the motion of an aircraft;
planning an aircraft route by an aircraft route planning and simulation module of the mission planning and fire control calculation platform according to the performance parameters of the aircraft and the position of a weapon launching point in a fire control calculation result, generating a route point of the aircraft flying to the weapon launching point to obtain an aircraft route planning result, simulating the aircraft flying to the weapon launching point, sending the aircraft route planning result to a simulation deduction display module, sending the aircraft movement information to a weapon management module, an efficiency evaluation module and a simulation deduction display module, wherein the simulation deduction display module displays the aircraft movement information and the aircraft route planning result, if the aircraft reaches the weapon launching point, the step 7 is carried out, otherwise, the aircraft flying to the weapon launching point is continuously simulated;
and 7: simulating weapon firing;
the task planning and fire control resolving table weapon management module simulates weapon emission parameter binding according to a task planning result, and simulates a weapon emission process until planned weapons are all emitted; after the firing is finished, sending the firing state of the weapon to a performance evaluation module, and entering step 8;
and 8: evaluating the efficiency;
and the performance evaluation module of the mission planning and fire control calculation table estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target during weapon launching and the carrier position, estimates the damage probability of the single target, sends the performance evaluation result to the simulation deduction display module, and the simulation deduction display module displays the performance evaluation result.
The invention has the beneficial effects that:
(1) aiming at the remote aerial support aerial carrier combat scene and the combat characteristics, the task planning and resolving process of the remote aerial support aerial carrier combat scene is simulated in a closed loop mode, and the remote aerial support aerial carrier combat flow and information interaction are verified;
(2) the simulation system adopts a modular design, decomposes the task planning and resolving of the remote aerial support aerial carrier into a plurality of modules such as situation threat assessment, task planning, fire control resolving, aerial carrier route planning, efficiency assessment and the like, is convenient for programming development and testing, has good expandability and can effectively verify the task planning and resolving algorithm;
(3) parameters of battlefield plans, airborne weapons and simulation entities in battle scenes can be quickly modified through a human-computer interface, and the user configuration is stored through a database, so that algorithm verification requirements under different battle scenes can be flexibly met;
(4) the battlefield situation in the simulation process is visually displayed, the planning and resolving results of all modules are displayed in an overlapping mode, and a user can conveniently verify the rationality and the correctness of a task planning and resolving algorithm.
Drawings
FIG. 1 is a diagram of an emulation system according to the present invention.
FIG. 2 is a schematic flow chart of a simulation method according to the present invention.
Detailed Description
The invention is further illustrated with reference to the following figures and examples.
(1) The mission planning and solving simulation system for the remote aerial support carrier comprises a battlefield force generation platform and a mission planning and fire control solving platform as shown in figure 1.
(2) The battlefield force generation platform is used as a main interactive interface for a user to configure a battle scene and manage a simulation process, and the user configures parameters of battlefield planning, airborne weapons and simulation entities in the battle scene and simulates the movement of enemy and my forces except the airborne weapons in the battlefield; and the mission planning and fire control resolving table simulates a remote aerial support carrier mission planning and fire control resolving process to carry out situation threat assessment, mission planning, fire control resolving, carrier air route planning and motion simulation, weapon emission control, efficiency assessment and simulation deduction display. The battlefield force generation platform is connected with the mission planning and fire control resolving platform through the Ethernet.
(3) The battlefield force generation platform is developed by adopting an object-oriented method based on a Qt framework and a Microsoft Access 2010 database. The battlefield force generation platform comprises a battlefield force management module, a database module and a network communication module.
The battlefield force management module reads the battle scenes stored in the database, including battlefield scenario, airborne weapons and simulation entity parameters, provides an operation interface for configuring the battle scenes for users, and provides a simulation deduction process management function. According to the configuration of a user on a battlefield planning and simulation entity, simulating the forces and movements of enemy and my arms, such as fighters, unmanned bureaucratic machines and targets of our party, simultaneously sending the fighting scenes configured by the user to a database module for storage, and sending the fighting scene configuration and the forces and movements information of the enemy and my arms to a mission planning and fire control resolving table through a network communication module.
The Database module provides an interface for accessing and operating the Microsoft Access 2010 Database based on ODBC (Open Database Connectivity) drivers. The database module stores the battle scene configured by the user, including battlefield scenario, airborne weapons and simulation entity parameters, into a database file in a data table form.
The network communication module is used for realizing communication between the battlefield force generation platform and the mission planning and fire control resolving platform based on a User Datagram Protocol (UDP), and sending the combat scene configuration and the enemy force movement information output by the battlefield force management module to the mission planning and fire control resolving platform.
(4) And the mission planning and fire control resolving platform is developed by adopting an object-oriented method based on a Qt framework. The mission planning and fire control calculation platform comprises a network communication module, a situation threat assessment module, a mission planning module, a fire control calculation module, an aircraft route planning and simulation module, a weapon management module, a performance assessment module and a simulation deduction display module.
The network communication module is used for realizing communication between the task planning and fire control resolving station and the battlefield force generation station based on UDP (user datagram protocol), receiving combat scene configuration and enemy force movement information sent by the battlefield force generation station network communication module, and distributing the received information to the other modules of the task planning and fire control resolving station.
The situation threat assessment module calculates situation threats of the targets relative to the aerial carrier and the fighter in the same party respectively according to the force and motion information of the enemy and the my, comprehensively assesses the threat degree of each target in the target formation, and sends situation threat assessment results to the task planning module and the simulation deduction display module.
The mission planning module completes fire planning and mission allocation according to the configuration of the airborne weapons, weapon parameters and situation threat assessment results in the operational scene, gives a launching mode suggestion, and sends the mission planning result to the fire control resolving module, the weapon management module and the simulation deduction display module.
The fire control calculation module calculates weapon attack areas, weapon launching points and weapon waypoints according to the operational scene configuration, the target motion information and the task planning result, and sends the fire control calculation result to the carrier route planning and simulation module, the weapon management module and the simulation deduction display module.
The carrier route planning and simulation module generates a route point of the carrier flying to the weapon launching point according to the carrier performance parameters and the position of the weapon launching point in the fire control calculation result, simulates the carrier flying to the weapon launching point, sends the carrier route planning result to the simulation deduction display module, and sends the carrier motion information to the weapon management module, the efficiency evaluation module and the simulation deduction display module.
The weapon management module simulates weapon state display and weapon emission control processes, simulates weapon emission parameter binding according to a task planning result, and judges whether the carrier reaches a weapon emission point according to carrier motion information and a fire control calculation result. And after the carrier reaches the weapon launching point, simulating the weapon launching process and sending the weapon launching state to the efficiency evaluation module.
After the weapon is launched, the performance evaluation module estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target and the carrier position during weapon launching, estimates the damage probability of the single target, and sends the performance evaluation result to the simulation deduction display module.
And the simulation deduction display module displays the two-dimensional battlefield environment and the forces of the enemy and my arms in the simulation process and displays the task planning and resolving results in the fighting simulation deduction process.
(5) As shown in fig. 2, the mission planning and solution simulation method for a remote aerial support carrier according to the present invention is implemented by the simulation system, and specifically includes the following steps:
step 1: and connecting the database. And the battlefield force generation database module completes the connection initialization of database files and reads the battle scenes stored in the database. And (5) after the database connection is completed, entering the step 2.
Step 2: configuring a battle scene and initializing a simulation deduction display. In the battlefield force generation platform, a battlefield force management module displays a battle scene stored in a database, a user configures parameters of battlefield planning, airborne weapons and simulation entities in the battle scene, and a network communication module sends the configured battle scene to a mission planning and fire control resolving platform. After the mission planning and fire control resolving station receives the battle scene, the simulation deduction display module initializes and displays the battlefield environment and the forces of the enemy and my arms, and the step 3 is carried out;
and step 3: and evaluating the situation threat. The task planning and fire control calculation station situation threat assessment module calculates situation threats of targets relative to the aerial carrier and the fighter of the same party respectively according to the soldier movement information of the enemy and the target performance parameters, comprehensively assesses the threat degree of each target in the target formation, and sends situation threat assessment results to the task planning module and the simulation deduction display module. The simulation deduction display module displays the situation threat assessment result and enters the step 4;
and 4, step 4: and (6) planning a task. And the task planning module of the task planning and fire control calculation platform completes fire planning and task allocation according to the configuration of airborne weapons, weapon parameters and situation threat assessment results in the operational scene, gives a launching mode suggestion, and sends the task planning result to the fire control calculation module, the weapon management module and the simulation deduction display module. The simulation deduction display module displays a task planning result and enters the step 5;
and 5: and (4) fire control calculation. And the fire control calculation module of the mission planning and fire control calculation platform calculates a weapon attack area, a weapon launching point and a weapon route point according to the operational scene configuration, the target motion information and the mission planning result, and sends the fire control calculation result to the carrier route planning and simulation module, the weapon management module and the simulation deduction display module. The simulation deduction display module displays the fire control calculation result and enters step 6;
step 6: planning the air route of the air carrier and simulating the movement of the air carrier. The mission planning and fire control calculation platform carrier air route planning and simulation module generates an air route point of the carrier flying to the weapon launching point according to the carrier performance parameters and the weapon launching point position in the fire control calculation result, simulates the carrier flying to the weapon launching point, sends the carrier air route planning result to the simulation deduction display module, and sends the carrier motion information to the weapon management module, the efficiency evaluation module and the simulation deduction display module. And the simulation deduction display module displays the position of the aircraft and the planning result of the aircraft route. If the carrier reaches the weapon launching point, entering step 7, otherwise, continuing simulating the carrier to fly to the weapon launching point;
and 7: simulating weapon firing. And the task planning and fire control resolving platform weapon management module simulates weapon emission parameter binding according to a task planning result, and simulates a weapon emission process until the planned weapons are all emitted. After the firing is finished, sending the firing state of the weapon to a performance evaluation module, and entering step 8;
and 8: and (5) evaluating the efficiency. And the task planning and fire control calculation station performance evaluation module estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target during weapon launching and the carrier position, estimates the damage probability of the single target, and sends the performance evaluation result to the simulation deduction display module. And the simulation deduction display module displays the efficiency evaluation result.
Claims (4)
1. A mission planning and resolving simulation system for a remote aerial support carrier comprises a battlefield force generation platform and a mission planning and fire control resolving platform, and is characterized in that:
the battlefield force generation platform is used for battle scene configuration, enemy and my force movement simulation and simulation process management except for the carrier, the task planning and fire control resolving platform is used for situation threat assessment, task planning, fire control resolving, carrier air route planning and movement simulation, weapon emission control, efficiency assessment and simulation deduction display, and the battlefield force generation platform is connected with the task planning and fire control resolving platform through the Ethernet.
2. The mission planning and solution simulation system for a remote airborne support vehicle according to claim 1, wherein:
the battlefield force generation platform comprises a battlefield force management module, a database module and a network communication module;
the battle field weaponry management module reads the battle scenes stored in the database, provides an operation interface for configuring battle field planning, airborne weapons and simulation entity parameters in the battle scenes for a user, provides a simulation deduction process management function, simulates the enemy and my weaponry movement except the carrier, and stores the battle scenes configured by the user into the database module in the specific process of firstly reading the battle scenes in the database and displaying the battle scenes in the operation interface for the user to modify;
the database module provides an interface for accessing and operating the database, and stores the battle scene configured by the user in a database file;
the network communication module realizes communication between the battlefield force generation platform and the mission planning and fire control resolving platform and sends fighting scene configuration and enemy force movement information in the fighting simulation process.
3. The mission planning and solution simulation system for a remote airborne support vehicle according to claim 1, wherein:
the mission planning and fire control calculation platform comprises a network communication module, a situation threat assessment module, a mission planning module, a fire control calculation module, an aircraft air route planning and simulation module, a weapon management module, a performance assessment module and a simulation deduction display module;
the network communication module realizes communication between the task planning and fire control resolving station and the battlefield force generating station, receives battle scene configuration and enemy force movement information in a battle simulation process, and distributes the received information to other modules of the task planning and fire control resolving station;
the situation threat assessment module calculates situation threats of the targets relative to the aerial carrier and the fighter in the same party respectively according to the force and motion information of the enemy and the my, comprehensively assesses the threat degree of each target in the target formation, and sends situation threat assessment results to the task planning module and the simulation deduction display module;
the task planning module completes fire planning and task allocation according to the configuration of airborne weapons, weapon parameters and situation threat assessment results in the operational scene, gives a launching mode suggestion, and sends the task planning results to the fire control resolving module, the weapon management module and the simulation deduction display module;
the fire control calculation module calculates a weapon attack area, a weapon launching point and a weapon waypoint according to the operational scene configuration, the target motion information and the task planning result, and sends the fire control calculation result to the carrier route planning and simulation module, the weapon management module and the simulation deduction display module;
the aircraft route planning and simulation module generates an aircraft route point of the aircraft flying to the weapon launching point according to the aircraft performance parameters and the position of the weapon launching point in the fire control calculation result, simulates the aircraft flying to the weapon launching point, sends the aircraft route planning result to the simulation deduction display module, and sends the aircraft motion information to the weapon management module, the efficiency evaluation module and the simulation deduction display module;
the weapon management module simulates weapon state display and weapon emission control processes, simulates weapon emission parameter binding according to a task planning result, judges whether the carrier reaches a weapon emission point or not according to carrier motion information and a fire control calculation result, simulates a weapon emission process after the carrier reaches the weapon emission point, and sends the weapon emission state to the efficiency evaluation module;
after the weapon is launched, the efficiency evaluation module estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target and the aircraft carrier position when the weapon is launched, estimates the damage probability of the single target, and sends the efficiency evaluation result to the simulation deduction display module;
the simulation deduction display module displays a two-dimensional battlefield environment and forces of enemy and my arms in the simulation process and displays a task planning and resolving result in the fighting simulation deduction process.
4. An implementation of the mission planning and solution simulation system for a remote airborne support vehicle according to claim 1, comprising the following steps:
step 1: connecting a database;
the battlefield force generation database module completes database file connection initialization, reads the battle scene stored in the database, and enters step 2 after database connection is completed;
step 2: configuring a battle scene and initializing simulation deduction display;
in a battlefield force generation platform, a battlefield force management module displays a battlefield scene stored in a database, a user configures parameters of battlefield planning, airborne weapons and simulation entities in the battlefield, a network communication module sends the configured battlefield scene to a mission planning and fire control resolving platform, and after the mission planning and fire control resolving platform receives the battlefield scene, a simulation deduction display module initializes and displays a battlefield environment and forces of enemy and my, and the step 3 is entered;
and step 3: assessing situation threats;
a situation threat assessment module of the task planning and fire control resolving station calculates situation threats of targets relative to the aerial carrier and the fighter of the party respectively according to the force and motion information of the enemy and considering target performance parameters, comprehensively assesses the threat degree of each target in the target formation to obtain a situation threat assessment result, sends the situation threat assessment result to a task planning module and a simulation deduction display module, displays the situation threat assessment result by the simulation deduction display module, and enters step 4;
and 4, step 4: planning a task;
a task planning module of the task planning and fire control calculation table finishes fire planning and task allocation according to the configuration of airborne weapons, weapon parameters and situation threat assessment results in an operational scene, gives weapons required by different emission frequencies and emission mode suggestions that each emission frequency should adopt simultaneous emission or continuous emission according to the fire planning and task allocation results and by considering emission constraints, finally obtains a task planning result, sends the task planning result to a fire control calculation module, a weapon management module and a simulation deduction display module, and the simulation deduction display module displays the task planning result and enters step 5;
and 5: calculating fire control;
calculating a weapon attack area, a weapon launching point and a weapon waypoint by a fire control calculation module of the mission planning and fire control calculation table according to the operational scene configuration, the target motion information and the mission planning result to obtain a fire control calculation result, sending the fire control calculation result to a carrier route planning and simulation module, a weapon management module and a simulation deduction display module, displaying the fire control calculation result by the simulation deduction display module, and entering the step 6;
step 6: planning an aircraft route and simulating the motion of an aircraft;
planning an aircraft route by an aircraft route planning and simulation module of the mission planning and fire control calculation platform according to the performance parameters of the aircraft and the position of a weapon launching point in a fire control calculation result, generating a route point of the aircraft flying to the weapon launching point to obtain an aircraft route planning result, simulating the aircraft flying to the weapon launching point, sending the aircraft route planning result to a simulation deduction display module, sending the aircraft movement information to a weapon management module, an efficiency evaluation module and a simulation deduction display module, wherein the simulation deduction display module displays the aircraft movement information and the aircraft route planning result, if the aircraft reaches the weapon launching point, the step 7 is carried out, otherwise, the aircraft flying to the weapon launching point is continuously simulated;
and 7: simulating weapon firing;
the task planning and fire control resolving table weapon management module simulates weapon emission parameter binding according to a task planning result, and simulates a weapon emission process until planned weapons are all emitted; after the firing is finished, sending the firing state of the weapon to a performance evaluation module, and entering step 8;
and 8: evaluating the efficiency;
and the performance evaluation module of the mission planning and fire control calculation table estimates the damage probability of the single weapon to the single target according to the weapon launching state, the motion information of each target during weapon launching and the carrier position, estimates the damage probability of the single target, sends the performance evaluation result to the simulation deduction display module, and the simulation deduction display module displays the performance evaluation result.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113139697A (en) * | 2021-05-12 | 2021-07-20 | 中国人民解放军军事科学院评估论证研究中心 | Intelligent force correlation method based on combat simulation |
| CN113268865A (en) * | 2021-05-12 | 2021-08-17 | 中国人民解放军军事科学院评估论证研究中心 | Aircraft behavior modeling construction method based on regular flow chain |
| CN113536528A (en) * | 2021-05-14 | 2021-10-22 | 中国人民解放军军事科学院评估论证研究中心 | Early warning aircraft tactical behavior simulation method and system under non-convoy condition |
| CN113705102A (en) * | 2021-08-31 | 2021-11-26 | 湖南苍树航天科技有限公司 | Deduction simulation system, method, equipment and storage medium for sea-air cluster confrontation |
| CN114239305A (en) * | 2021-12-23 | 2022-03-25 | 南京雷电信息技术有限公司 | Battlefield situation scene simulation excitation system |
| CN116720330A (en) * | 2023-05-23 | 2023-09-08 | 中国舰船研究设计中心 | Unmanned equipment simulation test system |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106094566A (en) * | 2016-06-13 | 2016-11-09 | 江西洪都航空工业集团有限责任公司 | A kind of method for low cost universal ground experiment simulation carrier aircraft system |
| CN109658770A (en) * | 2019-01-24 | 2019-04-19 | 江苏前景信息科技有限公司 | People's air defense training's air situation simulation system |
| CN110488633A (en) * | 2019-08-29 | 2019-11-22 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of avionics weapon attacking test macro |
-
2020
- 2020-10-30 CN CN202011198177.9A patent/CN112308422A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106094566A (en) * | 2016-06-13 | 2016-11-09 | 江西洪都航空工业集团有限责任公司 | A kind of method for low cost universal ground experiment simulation carrier aircraft system |
| CN109658770A (en) * | 2019-01-24 | 2019-04-19 | 江苏前景信息科技有限公司 | People's air defense training's air situation simulation system |
| CN110488633A (en) * | 2019-08-29 | 2019-11-22 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of avionics weapon attacking test macro |
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| CN113139697A (en) * | 2021-05-12 | 2021-07-20 | 中国人民解放军军事科学院评估论证研究中心 | Intelligent force correlation method based on combat simulation |
| CN113268865A (en) * | 2021-05-12 | 2021-08-17 | 中国人民解放军军事科学院评估论证研究中心 | Aircraft behavior modeling construction method based on regular flow chain |
| CN113268865B (en) * | 2021-05-12 | 2022-02-22 | 中国人民解放军军事科学院评估论证研究中心 | Aircraft behavior modeling construction method based on regular flow chain |
| CN113536528A (en) * | 2021-05-14 | 2021-10-22 | 中国人民解放军军事科学院评估论证研究中心 | Early warning aircraft tactical behavior simulation method and system under non-convoy condition |
| CN113705102A (en) * | 2021-08-31 | 2021-11-26 | 湖南苍树航天科技有限公司 | Deduction simulation system, method, equipment and storage medium for sea-air cluster confrontation |
| CN114239305A (en) * | 2021-12-23 | 2022-03-25 | 南京雷电信息技术有限公司 | Battlefield situation scene simulation excitation system |
| CN114239305B (en) * | 2021-12-23 | 2022-10-11 | 南京雷电信息技术有限公司 | Battlefield situation scene simulation excitation system |
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