CN106250663B - A kind of Architecture simulation method based on quantum electronics description - Google Patents
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Abstract
The Architecture simulation method based on quantum electronics description that the present invention relates to a kind of, this method includes defining simulation model, time stepping method calculating is carried out to simulation model, and state update is carried out to simulation model, the present invention redefines factoid basis using quantum mechanical ideas, the basic calculating module for defining simulation model reads rule, form the emulation mode of a set of support QSS acceleration and multiple-limb predictive simulation, realize the parallel operation of time series emulation, multiple-limb simulation analysis can be carried out using parallel space time theory, multiple branches are created in simulation process, various possibilities are analyzed comprehensively, the emulation mode has the ability of multiple-limb emulation, it can be using any time as starting point, to the different result of decision, the influence of chance event is emulated.
Description
Technical field
The Architecture simulation method based on quantum electronics description that the present invention relates to a kind of, belongs to simulation technical field.
Background technique
In the simulation process of Weapon Equipment System confrontation, need to consider the body of integrated form under Information Condition, federal style
Be grade network-centric warfare feature, need on the basis of carrying out clear, accurate, flexibly modeling to complication system to confrontation between systems into
Row emulation.In existing Simulation & evaluation system, needs that analogue system function is further standardized and divided, be provided with
The specification process that the assessment preparation of iterative relation, operation, analysis and synthesis form.Current simulation model and system specifications stop
It in application level, does not stand and defines analogue system on the level that physics describes substantially, there are certain incompleteness, cause
A series of application problems, such as: Simulation Application system can not the thought of applied dynamics differential carry out time slice emulation,
It is difficult to realize multiple-limb emulation；It is incomplete for recording for emulation data；There are logic errors for the service logic of simulation model, read
Take or be utilized unreasonable input data etc..
Summary of the invention
It is an object of the invention to overcome the drawbacks described above of the prior art, a kind of system based on quantum electronics description is provided
Emulation mode, the emulation mode have the ability of multiple-limb emulation, can be using any time as starting point, to different decision knots
Fruit, chance event influence emulated, greatly reduce emulation data capacity requirement, significantly improve calculating speed, while can
The cheating and mistake occurred to effectively reduce simulation model in environment calculating process.Fundamentally provide unified emulation
The means of environment.
What above-mentioned purpose of the invention was mainly achieved by following technical solution:
A kind of Architecture simulation method based on quantum electronics description, includes the following steps:
(1), simulation model is defined, i.e., the attribute to simulation model in simulation space is defined, including objective attribute
With subjective attribute, the objective attribute is the description to simulation model physical state, and the subjective attribute is in simulation model
The description of portion's logic；
(2), time stepping method calculating is carried out to simulation model, and state update is carried out to simulation model, specifically included as follows
Step:
(2.1), simulation model is initialized, specifically includes and runs relied on hardware resource progress to simulation model
Configure, the type of simulation model be defined, in simulation model application program generate simulation model variable data structure,
Between configuration simulation model mutually distribution subscription relationship required for read status information, simulation model example is initialized and to
The state of simulation model assigns initial value；
(2.2), time stepping method calculating is carried out to simulation model, the time stepping method calculating process successively includes: state point
Branch switching, Effect under external electric field calculate, sensor Sn is calculated, controller Cn is calculated and actuator calculates；
(2.3) calculated result of sensor, controller and actuator is subjected to state update to simulation model.
In the above-mentioned Architecture simulation method based on quantum electronics description, simulation model physical state includes in step (1)
Position, posture, speed, inertia, quality, angular speed, ROE state, flight operating condition, fuel quantity, ammunition, infrared target characteristic and
Electromagnetic target characteristic.
In the above-mentioned Architecture simulation method based on quantum electronics description, simulation model internal logic includes in step (1)
The all properties of event flag position and Cognitive Spaces, the event flag position include detection result, estimation result, conjecture result,
It is apprised of result, drives order, combat order and information transfer；The Cognitive Spaces refer to simulation model for simulated world
Understanding is formed by attribute space, and Cognitive Spaces information cannot directly be used by the example other than the simulation model example.
In the above-mentioned Architecture simulation method based on quantum electronics description, Cognitive Spaces include the simulation object recognized
The attribute of attribute and the simulated world recognized, wherein the attribute of the simulation object recognized includes the simulation object recognized
The Cognitive Spaces of objective status and the simulation object recognized, the attribute of the simulated world recognized include the outfield ginseng of pre- bookbinding
Several and preset physical principle.
In the above-mentioned Architecture simulation method based on quantum electronics description, in step (2.2) is carried out to simulation model the time
The specific method of propulsion includes the following steps:
(2.2.1), branches of states switching is carried out, defined calculating is specially entered according to the operating condition flag bit of simulation model
Branch, the operating condition flag bit are a variable in simulation model state vector；
(2.2.2), Effect under external electric field calculating is carried out in the defined calculating branch, calculated by the way of field,
I.e. specific state has the value uniquely determined in specific field, specific as follows:
F=f (AT)；
Wherein: F is Effect under external electric field suffered by simulation model example, comprising stress, injures probability and detection probability；ATFor T
The simulation model objective status attribute at moment；F () is the calculating function in outfield；
The Effect under external electric field F calculated in (2.2.3), calculating branch and step (2.2.2) specified in step (2.2.1)
Under, successively carry out sensor calculating, controller calculates and actuator calculates；
(2.2.4), according to the calculated result of sensor, controller and actuator in step (2.2.3) to simulation model into
Row state updates, and completes a time stepping method and calculates, and return step (2.2.1), the time stepping method for carrying out next period calculates.
In the above-mentioned Architecture simulation method based on quantum electronics description, sensor is calculated in step (2.2.3), i.e., to spy
The calculating of result On is surveyed, specific as follows:
On=Sn (T1, T2...TM)
Wherein: Sn () is the calculating function of sensor n, T1, T2...TMRespectively the 1st, the 2nd ... m-th quilt
The state of detected object, On are the detection results of sensor Sn, and form is simulated events.
In the above-mentioned Architecture simulation method based on quantum electronics description, controller is calculated in step (2.2.3), i.e., by T
The Cognitive Spaces R at momentTIt is updated to the Cognitive Spaces R at T+1 momentT+1, during time stepping method each time, controller according to
Permission Levels are successively settled accounts, and are calculated since the minimum controller C1 of permission, until calculating the highest controller Cn of permission
Until, specific formula is as follows:
RT+1=Cn (Cn-1 (... C2 (C1 (RT, M1T、M2T....MnT), M1T、M2T....MnT), M1T、
M2T....MnT), M1T、M2T....MnT)
Wherein: RTFor the Cognitive Spaces at T moment, RT+1For the Cognitive Spaces at T+1 moment, Cn () is controller logic calculating
Function, M1T、M2T....MnTFor whole subjective attribute events that T moment simulation model example receives, n is nonnegative integer.
In the above-mentioned Architecture simulation method based on quantum electronics description, actuator is calculated in step (2.2.3), that is, is emulated
The publication for the subjective attribute event that the update of model objective status attribute and simulation model generate, specifically includes the following steps:
(2.2.3.1), it is resolved according to the objective status attribute and Cognitive Spaces value of simulation model, phantom
It is specific as follows in the state value of time stepping method target point each time:
AT+1=Tick (AT,RT+1)
Wherein: RT+1For the Cognitive Spaces at T+1 moment, ATFor the simulation model objective status attribute at T moment, AT+1For T+1
The simulation model objective status attribute at moment, Tick () are the resolving function of actuator；
(2.2.3.2) is according to the simulation model objective status attribute A at T+1 momentT+1Field caused by simulation model is carried out
It updates；
(2.2.3.3), the value R according to the Cognitive Spaces at T+1 momentT+1, simulation model is issued in the secondary event progradation
The subjective attribute event of middle generation.
Compared with prior art, the present invention has the following advantages:
(1), the present invention redefines factoid basis, it is specified that the basic meter of simulation model using quantum mechanical ideas
It calculates module and reads rule, a set of support QSS of formation accelerates and the emulation mode of multiple-limb predictive simulation, realizes that time series emulates
Parallel operation can carry out multiple-limb simulation analysis using parallel space time theory, multiple branches be created in simulation process, comprehensively
Various possibilities are analyzed, which has the ability of multiple-limb emulation, can determine using any time as starting point to difference
Plan result, chance event influence emulated.
(2), the data record of emulation mode of the present invention reaches physically complete degree, therefore its data record is complete
, the playback of analogue system can be segmented according to the chance event and decision event of emulation, in each segmentation no longer
Playback of data but re-start emulation.This characteristic can greatly reduce the capacity requirement of emulation data.
(3), emulation mode of the present invention can apply the side QSS during actuator each time calculates and emulates playback
Method realizes parallelization processing, significantly improves calculating speed.
(4), emulation mode strict regulations of the present invention outfield (environment) calculation of effect mode, can effectively reduce emulation mould
The cheating and mistake that type occurs in environment calculating process fundamentally provide the means of unified simulated environment.
(5), the strict regulations of the present invention reading permission of sensor, has standardized sensor Simulation process；Stringent rule simultaneously
The operation logic for having determined controller allows simulation model using complicated controller model.
Detailed description of the invention
Fig. 1 is that objective attribute describes schematic diagram in simulation model of the present invention；
Fig. 2 is that subjective attribute describes schematic diagram in simulation model of the present invention, and wherein Fig. 2 a is that subjective attribute event description is shown
It is intended to；Fig. 2 b is that Cognitive Spaces describe schematic diagram.
Fig. 3 is emulation mode process schematic of the present invention.
Specific embodiment
Further detailed description is done to the present invention in the following with reference to the drawings and specific embodiments:
The present invention is based on the Architecture simulation methods of quantum electronics description, describe Simulation Application system each using state vector
The state at a moment is promoted using the process description simulation time of state transfer.The attribute type for having combed model of system, definition
Objective attribute and supervisor's attribute.Define the basic procedure of model application, it is determined that externally magnetic field effect calculates, sensor calculates,
The basic steps such as controller calculates, actuator calculates are, it is specified that each step limits the read-write of state.Construct a trocar
To the complete description system of System-of-systems Combat Simulation.Basic logic relationship and cyberspace scenario based on model reality may be implemented
The configuration of dynamic generation distribution subscription can use QSS emulation mode and carry out emulation final states calculating, realizes that time series emulation is parallel
Operation can carry out multiple-limb simulation analysis using parallel space time theory, multiple branches are created in simulation process, are analyzed comprehensively
Various possibilities.
In the Simulation Application system changed over time at one, the state of each moment analogue system is indicated with state.
State vector of the simulated world at the T moment includes value of the attribute at the T moment of each simulation model.
The attribute of simulation model includes two classes:
One kind is the description (objective attribute) to model physical state itself, is a kind of objective information, all values
Feasible zone is referred to as the real space.The physical state of model itself includes: the attributes such as position, speed, posture, weight, carried charge.Visitor
It sees attribute and meets orthogonal, complete requirement.It is objective that the physical quantity that stress etc. describes multiple model direct interactions is not belonging to model
Attribute, effect are calculated by field-effect and are realized.The information in outfield is safeguarded by emulation platform is unified.
If Fig. 1 is that objective attribute describes schematic diagram in simulation model of the present invention, simulation model itself physics shape as seen from the figure
State includes position, posture, speed, inertia, quality, angular speed, ROE state, flight operating condition, fuel quantity, ammunition, infrared target
Characteristic and electromagnetic target characteristic.
It is another kind of to be divided into the description to model internal logic (subjective attribute), it is a kind of subjective information of model, owns
The feasible zone of value is referred to as Cognitive Spaces.Model internal logic information includes all categories of event flag position and Cognitive Spaces
Property.Cognitive Spaces refer to that simulation model is formed by attribute space for the understanding of simulated world.Cognitive Spaces information cannot be by
Example other than this example is directly used.
It is illustrated in figure 2 subjective attribute in simulation model of the present invention and describes schematic diagram, wherein Fig. 2 a is subjective attribute event
Schematic diagram is described；Fig. 2 b be Cognitive Spaces schematic diagram is described, as seen from the figure event flag position include detection result, estimation result,
Conjecture result is apprised of result, drives order, combat order and information transfer；Cognitive Spaces refer to simulation model for emulation
The understanding in the world is formed by attribute space, and Cognitive Spaces information cannot directly be transported by the example other than this simulation model example
With.
The Cognitive Spaces include the attribute of the attribute of the simulation object recognized and the simulated world recognized, wherein by
The attribute of the simulation object of cognition includes recognizing for the objective status of the simulation object whole recognized and the simulation object recognized
Know space, the attribute of the simulated world recognized includes and the outer field parameters bound in advance and preset physical principle.
It is illustrated in figure 3 emulation mode process schematic of the present invention, the present invention is based on the Architecture simulations of quantum electronics description
Method specifically comprises the following steps:
(1), simulation model is defined, i.e. the attribute to simulation model in simulation space carries out complete definition, including visitor
Attribute and subjective attribute are seen, the objective attribute is the description to simulation model physical state itself, and the subjective attribute is pair
The description of simulation model internal logic.
(2), time stepping method calculating is carried out to simulation model, the calculating is carried out in a manner of state transfer, and to emulation mould
Type carries out state update, and the specific method is as follows:
(2.1), simulation model is initialized, specifically includes and runs relied on hardware resource progress to simulation model
Configure, the type of simulation model be defined, in simulation model application program generate simulation model variable data structure,
Between configuration simulation model mutually distribution subscription relationship required for read status information, simulation model example is initialized and to
The state of simulation model assigns initial value；
(2.2), time stepping method calculating is carried out to simulation model, time stepping method is a cyclic process, each logical time
It is calculated when propulsion primary.It is calculated according to branches of states switching, Effect under external electric field, sensor Sn calculates (n is natural number), controller Cn
Calculate (n is natural number), the permanent order that actuator calculates executes.
Specific method includes the following steps:
(2.2.1), branches of states switching is carried out first, specially according to as defined in the entrance of the operating condition flag bit of simulation model
Branch is calculated, the operating condition flag bit is a variable in simulation model state vector；
(2.2.2), Effect under external electric field calculating is carried out in the defined calculating branch, calculated by the way of field,
I.e. specific state has the value uniquely determined in specific field, and specific formula for calculation is as follows:
F=f (AT)；
Wherein: wherein: F is Effect under external electric field suffered by simulation model example, comprising stress, injures probability and detection probability；
ATFor the simulation model objective status attribute at T moment；F () is the calculating function in outfield, such as gravitational field or electric field express function.
Effect under external electric field calculating process resolves all Physical interactions that model is received, and is calculated by the way of field, i.e., special
Fixed state has the value uniquely determined in specific field.In simulation process, gravity, aerodynamic effects such as injure at the physics
Interaction is all made of this mode and realizes.All simulation models can be used same set of external field environment and calculate function library, realize
The unification of environmental model in Simulation Application system.
The Effect under external electric field F calculated in (2.2.3), calculating branch and step (2.2.2) specified in step (2.2.1)
Under, successively carry out sensor calculating, controller calculates and actuator calculates；
(2.2.3.1), wherein sensor calculate, i.e. the calculating to detection result On, specific formula is as follows:
On=Sn (T1, T2...TM)
Wherein: Sn () is the calculating function of sensor n, T1, T2...TMRespectively the 1st, the 2nd ... m-th quilt
The state of detected object, On are the detection results of sensor Sn, and form is simulated events.
Sensor calculating is detection process of the sensor for simulated world of simulation model, this is can uniquely to subscribe to it
The computing unit of his model objective attribute information.Each simulation model can be equipped with n sensor.In time stepping method each time
It successively calculates in the process.
(2.2.3.2), controller calculate, i.e., by the Cognitive Spaces R at T momentTIt is updated to the Cognitive Spaces R at T+1 momentT+1,
During time stepping method each time, controller is successively settled accounts according to Permission Levels, is calculated since the minimum C1 of permission,
Until calculating permission highest controller Cn, specific formula is as follows:
RT+1=Cn (Cn-1 (... C2 (C1 (RT, M1T、M2T....MnT), M1T、M2T....MnT), M1T、
M2T....MnT), M1T、M2T....MnT)
Wherein: RTFor the Cognitive Spaces at T moment, RT+1For the Cognitive Spaces at T+1 moment, Cn () is controller logic calculating
Function, M1T、M2T....MnTFor whole subjective attribute events that the T moment simulation model example receives, n is nonnegative integer.
During time stepping method each time, controller is successively settled accounts according to Permission Levels, the C1 minimum from permission
Start to execute, until having executed permission highest controller Cn.Wherein in the Ci calculating process of each level, require to examine
Consider the related subjective attribute event Mn of moment wholeT, while updating Cognitive Spaces RT.In the Ci+1 calculating process of next level
Using the updated Cognitive Spaces R of upper one layer of machine CiT, remaining related subjective attribute event M1T、M2T....MnTIt is constant.
Controller calculating emulates the subjective characteristic of model, handles the event information of model, constructs and safeguard model
Cognitive Spaces.Controller calculating cannot be written and read the objective attribute of any model.In time stepping method each time
In the process, controller is successively settled accounts according to Permission Levels, is executed since the minimum C1 of permission, until having executed permission most
Until high controller Cn.
(2.2.3.3), actuator calculate, i.e. the master of the update of simulation model objective status attribute and simulation model generation
The publication of attribute event is seen, specifically includes the following steps:
(2.2.3.3.1), it is resolved according to the objective status attribute and Cognitive Spaces value of simulation model, computer sim- ulation mould
Type time stepping method target point each time state value, specific formula is as follows:
AT+1=Tick (AT,RT+1)
Wherein: RT+1For the Cognitive Spaces at T+1 moment, ATFor the simulation model objective status attribute at T moment, AT+1For T+1
The simulation model objective status attribute at moment, Tick () are the resolving function of actuator, such as dynamics integral.
(2.2.3.3.2), the simulation model objective status attribute A according to the T+1 momentT+1To field caused by simulation model
It is updated；
(2.2.3.3.3), the value R according to the Cognitive Spaces at T+1 momentT+1, issue simulation model and be advanced in the secondary event
The subjective attribute event generated in journey.
(2.2.4), according to the calculated result of sensor, controller and actuator in step (2.2.3) to simulation model into
Row state updates, and completes a time stepping method and calculates, and return step (2.2.1), the time stepping method for carrying out next period calculates.
Embodiment 1
It is described by taking an area-defense system confronting simulation application system as an example, which includes infrared guidance air defense
Guided missile and attack two class simulation model of operational aircraft.
Using the Architecture simulation system provided by the invention based on quantum mechanics thought, implementation steps are as follows:
Application model definitional language, defines the states model of this system, and the objective attribute of this system includes the work of air defence missile
Condition flag bit, position, speed, posture, target property, operating condition flag bit, position, the speed, posture of operational aircraft；This system
Supervisor's attribute includes that MISSILE LAUNCHING instruction, the target information of guided missile detection, guided missile are guidanceed command.
Process according to Fig. 3 writes two class simulation models, designs a specific experiment sample according to scenario, the sample
Initial state information includes the value of whole variable described in above-mentioned state.Initial time is set as 0 second, emulation end time is 100 seconds,
Simulation step length 1 second.
Operation is respectively started in two model programs, represents a guided missile example and an exemplary aircraft.
Two model programs carry out hardware platform initialization, set hardware configuration information；
Two model programs are instantiated as aircraft class and guided missile class according to scenario respectively；
Two model programs generate model object respectively；
Position, speed, posture and the target property information of guided missile example subscription exemplary aircraft.Exemplary aircraft without sensor,
Do not subscribe to external information.
Model instance initialization, the state according to scenario information to two model instances assign initial value.
Simulation time starts to promote, since 0 second, guided missile operating condition be it is standby, aircraft operating condition be cruise.Guided missile is in standby work
Under condition, sensor carries out visibility and sentences according to the position of aircraft, posture and target property information and the position of itself, posture information
It is disconnected；If visibility judge is very, to export detection event, ID and location information comprising target；If visibility judge is
Vacation, controller are failure to actuate, and actuator is failure to actuate.
30 seconds, aircraft entered guided missile detection range, and guided missile sensor exports detection event；STT missile device is according to detection thing
Part establishes object module in Cognitive Spaces, sets solution of fire control state for the subsequent time operating condition in Cognitive Spaces；It executes
Device is arranged according to the subsequent time operating condition in Cognitive Spaces sets solution of fire control state for operating condition flag bit.
Guided missile model enters solution of fire control branches of states within 31 seconds, which calculates without sensor；Controller enters fire control solution
Calculation state calculates launch data, is stored in Cognitive Spaces；It completes to be set as emitting by the subsequent time operating condition of Cognitive Spaces after calculating
Flight；Actuator sets transmitting flight for operating condition according to the setting of Cognitive Spaces, calculates subsequent time position according to launch data
Set velocity gesture.
50 seconds guided missiles fly according to launch data to aircraft vicinity, and actuator is according to the setting of launch data in Cognitive Spaces
Operating condition is switched to explosion, field data table is injured in update.The probability function that field data table is a three-dimensional space is injured, each
What simulation model inquired oneself present position in time stepping method each time injures field value, if being not 0 according to injure probability into
Row probabilistic simulation decides whether to be set as destroying by operating condition according to simulation result.
The field computation result of injuring of 51 seconds aircrafts is very that operating condition is arranged to destroy.
The above, optimal specific embodiment only of the invention, but scope of protection of the present invention is not limited thereto,
In the technical scope disclosed by the present invention, any changes or substitutions that can be easily thought of by anyone skilled in the art,
It should be covered by the protection scope of the present invention.
The content that description in the present invention is not described in detail belongs to the well-known technique of professional and technical personnel in the field.
Claims (7)
1. a kind of Architecture simulation method based on quantum electronics description, it is characterised in that include the following steps:
(1), simulation model is defined, i.e. the attribute to simulation model in simulation space is defined, including objective attribute and master
Attribute is seen, the objective attribute is the description to simulation model physical state, and the subjective attribute is to patrol simulation model inside
The description collected；
(2), time stepping method calculating is carried out to simulation model, and state update is carried out to simulation model, specifically comprised the following steps:
(2.1), simulation model is initialized, specifically includes the hardware resource relied on to simulation model operation and matches
Set, the type of simulation model be defined, in simulation model application program generate simulation model variable data structure, match
Distribution subscription relationship required for mutual read status information between simulation model is set, simulation model example is initialized and to imitative
The state of true mode assigns initial value；
(2.2), time stepping method calculating is carried out to simulation model, the time stepping method calculating process successively includes: that branches of states is cut
It changes, Effect under external electric field calculates, sensor Sn is calculated, controller Cn is calculated and actuator calculates；
(2.3) calculated result of sensor, controller and actuator is subjected to state update to simulation model；
The specific method for carrying out time stepping method to simulation model in the step (2.2) includes the following steps:
(2.2.1), branches of states switching is carried out, defined calculate specially is entered according to the operating condition flag bit of simulation model and is divided
Branch, the operating condition flag bit are a variable in simulation model state vector；
(2.2.2), it carries out Effect under external electric field calculating in the defined calculating branch, is calculated by the way of field, i.e., it is special
Fixed state has the value uniquely determined in specific field, specific as follows:
F=f (AT)；
Wherein: F is Effect under external electric field suffered by simulation model example, comprising stress, injures probability and detection probability；ATFor the T moment
Simulation model objective status attribute；F () is the calculating function in outfield；
(2.2.3), specified in step (2.2.1) calculating branch and step (2.2.2) in calculate Effect under external electric field F it
Under, successively carry out sensor calculating, controller calculates and actuator calculates；
(2.2.4), shape is carried out to simulation model according to the calculated result of sensor, controller and actuator in step (2.2.3)
State updates, and completes a time stepping method and calculates, and return step (2.2.1), the time stepping method for carrying out next period calculates.
2. a kind of Architecture simulation method based on quantum electronics description according to claim 1, it is characterised in that: the step
Suddenly in (1) simulation model physical state include position, posture, speed, inertia, quality, angular speed, ROE state, flight operating condition,
Fuel quantity, ammunition, infrared target characteristic and electromagnetic target characteristic.
3. a kind of Architecture simulation method based on quantum electronics description according to claim 1, it is characterised in that: the step
Suddenly in (1) simulation model internal logic include event flag position and Cognitive Spaces all properties, the event flag position includes
Detection result, estimation result guess result, are apprised of result, drive order, combat order and information transfer；The cognition is empty
Between refer to that simulation model is formed by attribute space for the understanding of simulated world, Cognitive Spaces information cannot be by the simulation model
Example other than example is directly used.
4. a kind of Architecture simulation method based on quantum electronics description according to claim 3, it is characterised in that: described to recognize
Know that space includes the attribute of the attribute of the simulation object recognized and the simulated world recognized, wherein the simulation object recognized
Attribute include the objective status of the simulation object recognized and the simulation object recognized Cognitive Spaces, the emulation recognized
The attribute in the world include pre- bookbinding outer field parameters and preset physical principle.
5. a kind of Architecture simulation method based on quantum electronics description according to claim 1, it is characterised in that: the step
Suddenly sensor calculates in (2.2.3), i.e. the calculating to detection result On is specific as follows:
On=Sn (T1, T2…TM)
Wherein: Sn () is the calculating function of sensor n, T1, T2…TMRespectively the 1st, the 2nd ... m-th inspected object
State, On is the detection result of sensor Sn, and form is simulated events.
6. a kind of Architecture simulation method based on quantum electronics description according to claim 1, it is characterised in that: the step
Suddenly controller calculates in (2.2.3), i.e., by the Cognitive Spaces R at T momentTIt is updated to the Cognitive Spaces R at T+1 momentT+1, each
During secondary time stepping method, controller is successively settled accounts according to Permission Levels, is calculated since the minimum controller C1 of permission,
Until calculating permission highest controller Cn, specific formula is as follows:
RT+1=Cn (Cn-1 (... C2 (C1 (RT, M1T、M2T….MnT), M1T、M2T….MnT), M1T、M2T….MnT), M1T、
M2T….MnT)
Wherein: RTFor the Cognitive Spaces at T moment, RT+1For the Cognitive Spaces at T+1 moment, Cn () is that controller logic calculates function,
M1T、M2T….MnTFor whole subjective attribute events that T moment simulation model example receives, n is nonnegative integer.
7. a kind of Architecture simulation method based on quantum electronics description according to claim 1 or 5, it is characterised in that: institute
It states actuator in step (2.2.3) to calculate, i.e. the subjectivity of the update of simulation model objective status attribute and simulation model generation
The publication of attribute event, specifically includes the following steps:
(2.2.3.1), it is resolved according to the objective status attribute and Cognitive Spaces value of simulation model, phantom is every
The state value of time stepping method target point, specific as follows:
AT+1=Tick (AT,RT+1)
Wherein: RT+1For the Cognitive Spaces at T+1 moment, ATFor the simulation model objective status attribute at T moment, AT+1For the T+1 moment
Simulation model objective status attribute, Tick () are the resolving function of actuator；
(2.2.3.2) is according to the simulation model objective status attribute A at T+1 momentT+1Field caused by simulation model is carried out more
Newly；
(2.2.3.3), the value R according to the Cognitive Spaces at T+1 momentT+1, issue simulation model and produced in the secondary event progradation
Raw subjective attribute event.
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| CN103593516A (en) * | 2013-10-30 | 2014-02-19 | 中国运载火箭技术研究院 | Combat system modeling and simulation system |
| CN105812367A (en) * | 2016-03-15 | 2016-07-27 | 浙江神州量子网络科技有限公司 | Authentication system and authentication method of network access device in quantum network |
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| CN103593516A (en) * | 2013-10-30 | 2014-02-19 | 中国运载火箭技术研究院 | Combat system modeling and simulation system |
| CN105812367A (en) * | 2016-03-15 | 2016-07-27 | 浙江神州量子网络科技有限公司 | Authentication system and authentication method of network access device in quantum network |
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