CN111308907A - Automatic battle-level airplane simulation control method, control plug-in and simulation system - Google Patents
Automatic battle-level airplane simulation control method, control plug-in and simulation system Download PDFInfo
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Abstract
The application relates to an automatic battle-level aircraft simulation control method, which comprises the following steps: defining a plurality of sub-rules; each sub-rule is obtained by splitting an air combat rule; combining all the sub-rules to form a fighting rule; receiving aircraft simulation parameters; and outputting the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters. And, to an automatic engagement level aircraft simulation control plug-in, comprising: a plurality of sub-rule modules, each sub-rule module correspondingly defines a sub-rule; each sub-rule is obtained by splitting an air combat rule; the operation rule module is used for combining the sub-rules defined in each sub-rule module to form an operation rule; the simulation parameter receiving module is used for receiving aircraft simulation parameters; and the simulation control parameter output module outputs the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters. Furthermore, an autowarfare class aircraft simulation system with the above-described autowarfare class simulation control plug-in is concerned.
Description
Technical Field
The application belongs to the technical field of automatic battle-level airplane simulation experiments, and particularly relates to an automatic battle-level airplane simulation control method, a control plug-in and a simulation system.
Background
Modern air combat process is complicated, and the evaluation index is various, and the change of air combat situation has high randomness, needs a large amount of samples just can study out the law wherein.
Currently, the assessment of the operational effectiveness of the battle-level airplane is mainly completed by adopting a battle-level airplane simulation system shown in fig. 1, the simulation system adopts a distributed simulation framework and a plug-in type integration method, different functional models are integrated into the system in a plug-in form, agile development is supported, plug and play are realized, and the simulation test of the human-in-the-loop has the following defects:
1) due to the limitation of personnel, time, equipment and other factors, only a limited number of sample sizes can be obtained, and the complexity of air combat cannot be fully reflected on the basis of the sample sizes;
2) and artificial factors are introduced, so that the decision points of each pattern, including the aspects of shooting opportunity, selection of avoidance strategies and the like, and the reflection time are different, the influence of the artificial factors which cannot be ignored is contained in an experimental structure, and the interference is brought to the evaluation work.
The present application is made in view of the above-mentioned drawbacks of the prior art.
Disclosure of Invention
The present application is directed to an automatic warfare class aircraft simulation control method, control plug-in and simulation system, which overcome or alleviate at least one of the disadvantages of the prior art.
The technical scheme of the application is as follows:
on the one hand, the simulation control method for the automatic battle-level airplane is provided, and comprises the following steps:
defining a plurality of sub-rules; each sub-rule is obtained by splitting an air combat rule;
combining all the sub-rules to form a fighting rule;
receiving aircraft simulation parameters;
and outputting the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
In accordance with at least one embodiment of the present application, the air combat rules, which are applicable to the assessment of battle performance at the battle level, may be summarized in terms of operational use research results.
According to at least one embodiment of the present application, each sub-rule is obtained by splitting an air combat rule, specifically:
and splitting the air combat rules according to the combat process and the maneuver characteristics to obtain each sub-rule.
According to at least one embodiment of the present application, the plurality of sub-rules comprises: a war zone entering sub-rule, a target distribution sub-rule, a tracking lock sub-rule, a missile launching sub-rule, a guidance in sub-rule, an avoidance sub-rule, a departure sub-rule, a reentry sub-rule, and a battlefield exit sub-rule.
According to at least one embodiment of the present application, the sub-rules are combined to form a battle rule, specifically:
and logically combining the sub-rules according to the fighting efficiency evaluation requirement to form a fighting rule.
Another aspect provides an automatic engagement level aircraft simulation control plug-in, comprising:
a plurality of sub-rule modules, each sub-rule module correspondingly defines a sub-rule; each sub-rule is obtained by splitting an air combat rule;
the operation rule module is used for combining the sub-rules defined in each sub-rule module to form an operation rule;
the simulation parameter receiving module is used for receiving aircraft simulation parameters;
and the simulation control parameter output module outputs the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
According to at least one embodiment of the present application, the plurality of sub-rule modules includes:
entering a target war zone sub-rule module, and defining a war zone entering sub-rule;
the target distribution sub-rule module defines a target distribution sub-rule;
a tracking lock sub-rule module for defining a tracking lock sub-rule;
the missile launching rule module defines missile launching rules;
the middle leader rule module defines a middle leader rule;
the avoidance sub-rule module defines avoidance sub-rules;
a deionization rule module for defining a deionization sub-rule;
the reentry sub-rule module defines reentry sub-rules;
and the quit battlefield sub-rule module defines a quit battlefield sub-rule.
Still another aspect provides an automatic battle-level aircraft simulation system, comprising:
any one of the automatic warfare level simulation control plug-ins is used for receiving aircraft simulation parameters and outputting corresponding aircraft simulation control parameters;
the plurality of airplane function simulation plug-ins are used for outputting airplane simulation parameters, receiving airplane simulation control parameters and acting according to the airplane simulation control parameters.
According to at least one embodiment of the application, the plurality of aircraft function simulation plug-ins comprise at least a radar plug-in and a missile plug-in.
Drawings
FIG. 1 is a schematic diagram of a prior art engagement-level aircraft simulation system provided herein;
FIG. 2 is a schematic diagram of an automatic engagement level aircraft simulation control plug-in provided by an embodiment of the present application;
fig. 3 is a schematic diagram of an automatic engagement-level aircraft simulation system according to an embodiment of the present application.
Detailed Description
The present application will be described in further detail with reference to the following drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the relevant application and are not limiting of the application. It should be noted that, for convenience of description, only the portions related to the present application are shown in the drawings.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
It should be noted that in the description of the present application, the terms of direction or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are based on the directions or positional relationships shown in the drawings, which are merely for convenience of description, and do not indicate or imply that the device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present application. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
Furthermore, it should be noted that, in the description of the present application, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present application can be understood by those skilled in the art as the case may be.
The present application is described in further detail below with reference to fig. 1 to 3.
On the one hand, the simulation control method for the automatic battle-level airplane is provided, and comprises the following steps:
defining a plurality of sub-rules; each sub-rule is obtained by splitting an air combat rule;
combining all the sub-rules to form a fighting rule;
receiving aircraft simulation parameters;
and outputting the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
For the automatic battle-level aircraft simulation control method disclosed in the above embodiment, it can be understood by those skilled in the art that a plurality of sub-rules obtained by splitting the air battle rule are defined, and then the sub-rules are correspondingly combined to form a battle rule, and based on the battle rule and the received aircraft simulation parameters, aircraft simulation control parameters are output, so that the corresponding control of the battle-level aircraft simulation system can be realized based on the output aircraft simulation control parameters.
For the automatic battle-level aircraft simulation control method disclosed in the above embodiment, it can be further understood by those skilled in the art that the air battle rule is decomposed into a plurality of general sub-rules and defined, and the sub-rules can be correspondingly combined to form a battle rule according to the battle effectiveness evaluation requirement, so that the corresponding control is convenient and flexible.
For the automatic battle-level aircraft simulation control method disclosed in the above embodiment, it can be further understood by those skilled in the art that the uncertain human control is not introduced based on the corresponding control of the method on the battle-level aircraft simulation system, and the influence of unstable human factors can be eliminated.
In some alternative embodiments, the air combat rules may be summarized in terms of operational use research results, which are applicable to the assessment of operational effectiveness at the engagement level.
In some optional embodiments, each sub-rule is obtained by splitting an air combat rule, specifically:
and splitting the air combat rules according to the combat process and the maneuver characteristics to obtain each sub-rule.
In some optional embodiments, the plurality of sub-rules comprises: a war zone entering sub-rule, a target distribution sub-rule, a tracking lock sub-rule, a missile launching sub-rule, a guidance in sub-rule, an avoidance sub-rule, a departure sub-rule, a reentry sub-rule, and a battlefield exit sub-rule.
In some optional embodiments, the sub-rules are combined to form a battle rule, specifically:
and logically combining the sub-rules according to the fighting efficiency evaluation requirement to form a fighting rule.
Another aspect provides an automatic engagement level aircraft simulation control plug-in, comprising:
a plurality of sub-rule modules, each sub-rule module correspondingly defines a sub-rule; each sub-rule is obtained by splitting an air combat rule;
the operation rule module is used for combining the sub-rules defined in each sub-rule module to form an operation rule;
the simulation parameter receiving module is used for receiving aircraft simulation parameters;
and the simulation control parameter output module outputs the aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
For the automatic warfare-level aircraft simulation control plug-in unit of the dynamic warfare level disclosed in the above embodiment, as can be further understood by those skilled in the art, a plurality of sub-rules obtained by splitting the air warfare rule are defined by a plurality of sub-rule modules, the sub-rules defined in each sub-rule module are combined by the combat rule module to form a combat rule, the aircraft simulation parameter is received by the simulation parameter receiving module, the aircraft simulation control parameter is output by the simulation control parameter output module based on the combat rule and the aircraft simulation parameter, and corresponding control of the warfare-level aircraft simulation system is realized based on the aircraft simulation control parameter output module.
For the automatic warfare-level aircraft simulation control plug-in disclosed in the above embodiment, those skilled in the art can also understand that the plug-in can replace a human-in-the-loop control lever control plug-in the existing warfare-level aircraft simulation system to realize automatic control of the warfare-level aircraft simulation system, thereby avoiding introduction of uncertain artificial control and eliminating the influence of unstable artificial factors.
In some optional embodiments, the plurality of sub-rule modules comprises:
entering a target war zone sub-rule module, and defining a war zone entering sub-rule;
the target distribution sub-rule module defines a target distribution sub-rule;
a tracking lock sub-rule module for defining a tracking lock sub-rule;
the missile launching rule module defines missile launching rules;
the middle leader rule module defines a middle leader rule;
the avoidance sub-rule module defines avoidance sub-rules;
a deionization rule module for defining a deionization sub-rule;
the reentry sub-rule module defines reentry sub-rules;
and the quit battlefield sub-rule module defines a quit battlefield sub-rule.
Still another aspect provides an automatic battle-level aircraft simulation system, comprising:
any one of the automatic warfare level simulation control plug-ins is used for receiving aircraft simulation parameters and outputting corresponding aircraft simulation control parameters;
the plurality of airplane function simulation plug-ins are used for outputting airplane simulation parameters, receiving airplane simulation control parameters and acting according to the airplane simulation control parameters.
For the automatic engagement-level aircraft simulation system disclosed in the above embodiment, the automatic engagement-level simulation control plug-in replaces the human-in-the-loop joystick control plug-in the existing engagement-level aircraft simulation system, so that the introduction of uncertain artificial control is avoided, and the influence of unstable artificial factors can be eliminated.
In some optional embodiments, the plurality of aircraft function simulation plug-ins includes at least a radar plug-in, a missile plug-in.
So far, the technical solutions of the present application have been described in connection with the preferred embodiments shown in the drawings, but it is easily understood by those skilled in the art that the scope of the present application is obviously not limited to these specific embodiments. Equivalent changes or substitutions of related technical features can be made by those skilled in the art without departing from the principle of the present application, and the technical scheme after the changes or substitutions will fall into the protection scope of the present application.
Claims (6)
1. An automatic battle-level aircraft simulation control method is characterized by comprising the following steps:
defining a plurality of sub-rules; each sub-rule is obtained by splitting an air combat rule;
combining the sub-rules to form a fighting rule;
receiving aircraft simulation parameters;
and outputting aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
2. The method of automated engagement-level aircraft simulation control according to claim 1,
the plurality of sub-rules includes: a war zone entering sub-rule, a target distribution sub-rule, a tracking lock sub-rule, a missile launching sub-rule, a guidance in sub-rule, an avoidance sub-rule, a departure sub-rule, a reentry sub-rule, and a battlefield exit sub-rule.
3. An automatic engagement-level aircraft simulation control plug-in, comprising:
the system comprises a plurality of sub-rule modules, a plurality of application modules and a plurality of application modules, wherein each sub-rule module correspondingly defines a sub-rule; each sub-rule is obtained by splitting an air combat rule;
the operation rule module is used for combining the sub-rules defined in the sub-rule modules to form operation rules;
the simulation parameter receiving module is used for receiving aircraft simulation parameters;
and the simulation control parameter output module outputs aircraft simulation control parameters based on the combat rules and the aircraft simulation parameters.
4. The autowar-grade aircraft simulation control plug-in of claim 3,
a plurality of the sub-rule modules include:
entering a target war zone sub-rule module, and defining a war zone entering sub-rule;
the target distribution sub-rule module defines a target distribution sub-rule;
a tracking lock sub-rule module for defining a tracking lock sub-rule;
the missile launching rule module defines missile launching rules;
the middle leader rule module defines a middle leader rule;
the avoidance sub-rule module defines avoidance sub-rules;
a deionization rule module for defining a deionization sub-rule;
the reentry sub-rule module defines reentry sub-rules;
and the quit battlefield sub-rule module defines a quit battlefield sub-rule.
5. An automatic engagement-level aircraft simulation system, comprising:
the autowar-grade simulation control plug-in of any one of claims 3-4, configured to receive aircraft simulation parameters and output corresponding aircraft simulation control parameters;
and the plurality of airplane function simulation plug-ins are used for outputting the airplane simulation parameters, receiving the airplane simulation control parameters and acting according to the airplane simulation control parameters.
6. The automated warfare class aircraft simulation system of claim 5,
the plurality of airplane function simulation plug-ins at least comprise radar plug-ins and missile plug-ins.
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