CN109901626A - A kind of scouting strike integration data processing system and method - Google Patents
A kind of scouting strike integration data processing system and method Download PDFInfo
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- CN109901626A CN109901626A CN201910091361.4A CN201910091361A CN109901626A CN 109901626 A CN109901626 A CN 109901626A CN 201910091361 A CN201910091361 A CN 201910091361A CN 109901626 A CN109901626 A CN 109901626A
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Abstract
The invention belongs to air vehicle technique field, a kind of scouting strike integration data processing system and method are disclosed.Scouting strike integration data processing system includes technique preparation process module and execution flow of task module.High speed, which is scouted, hits integrated unmanned plane, is located at immediately ahead of unmanned plane according to target when strike, calculates and analyze the various parameters that unmanned plane executes strike task under the conditions of different flying heights, flying speed；Covering hits process with the scouting for meeting target, realizes attack precision on a surface target；When implementing strike on a surface target, integrated unmanned plane carry precision guided weapon is hit for scouting, captures target after the booting of air weapon target seeker, terminal guidance hands over to the next shift in realization.The present invention realizes target location algorithm design, position error distribution and attack precision analysis, it the abilities such as effectively improves the long-range strike of existing weaponry and equipment, high-speed maneuver and accurately injures, enhance my strategfic reconnaissance, attack and land-sea aviation integral defence capability of the army in future war.
Description
Technical field
The invention belongs to air vehicle technique field more particularly to a kind of scouting strike integration data processing system and sides
Method.
Background technique
Currently, the prior art commonly used in the trade is such that
In the high-tech IT-based warfare epoch, accurately battle reconnaissance information, remote intelligent commander and precision strike become
Determine the main element of war win and defeat.Unmanned plane has become the important optimal in structure in future war, more and more states
Family shows great interest to High Performance Unmanned Aerial Vehicle, and the unmanned plane of various models has been used in present war.It is micro-
Fusion robot technology that Mini-Unmanned Aerial Vehicles are the 1990s to be developed by the country such as U.S., advanced power with
The new concept weapon of the advanced technologies such as Push Technology, miniaturization technologies, not only in basic theory, design, manufacture and experimental technique
Etc. be revolutionary innovation, and revolutionary and subversive influence will be brought on the war mode of 21 century.
Missile-borne Small and micro-satellite is a kind of new concept weapon system, achievable precision strike, scouting, relayed communications, mesh
Mark instruction, battlefield damage effectiveness determine and the multiple-tasks such as interference.Its main feature is that: 1) forward position protective net can be directly passed through, is supported
Up to target reconnaissance area, speed is fast, and battlefield survival is strong；2) missile-borne unmanned plane is usually encapsulated in the fight of the body with drag parachute
In portion's packing tube, maintenance, maintenance, convenient transportation are quick；3) just voluntarily folding and expanding when flying to spot overhead, enables itself
Dynamical system, capacity usage ratio maximize；4) production, use cost are low, can be produced in batches on a large scale.
In conclusion problem of the existing technology is:
(1) existing weaponry and equipment has the long-range strike, high-speed maneuver and the accurate damage effect effect that strike target to be hoisted.It is right
The Long-range precision strike of target needs accurate intelligence support, and in most cases to the surveillance information of target proximity from
Deep space satellite detection result, accuracy is lower and timeliness is low, and the precision strike that can not be equipped for long-range strike provides real-time
High information.Therefore function will be scouted and weapon strike function is integrated on high-speed unmanned aerial vehicle, can be realized to real-time detecting
Target timely hit, without the support of other weapon platforms, increase information obtained by scouting timeliness and
The accuracy of long-range strike；Reduce the informational linkage between reconnaissance platforms and weapon support platform simultaneously, can greatly improve to mesh
The concealment of strike is marked, the destructiveness of electronic warfare and the network warfare is reduced.
(2) existing scout is hit more scoutings integrated on integrated unmanned plane and is not believed directly between strike module mostly
Breath transmitting connection, needs using terrestrial information command centre or Air Operation Center as transfer and carries out centralized control, can not
It realizes unmanned plane autonomous surveillance and is hit, summarized from the information fusion spied out between strike not logical enough with information exchange
Freely.It is to die or target that Impulse time window is very short is easy most preferably to beat because the complexity of information mutual communication is led to miss for slightly wink
Window is hit, more copes with fast-changing situation of battlefield without condition to make in real time accurately reaction.
(3) existing to focus on unmanned plane for needs for scouting or examining dozen autonomous control technology of integrated unmanned plane more
The reconnaissance stage (including mission planning, target identification, battlefield detection and Situation Assessment etc.) of the target of strike and determining target
Tracking investigation stage (including track planning and strike path planning etc.) afterwards, but for the specific strike side of strike stage
The middle end guide mode research of the selection and combination and weapon module of formula is less；And after being hit, for target
Strike effect needs are confirmed by commanding in the rear center and are chosen whether to carry out two-hit according to strike effect, are easy to miss rapidly
Destroy the chance of target, it is difficult to reach the desired effect that long range penetration scouts strike.
Solve the difficulty and meaning of above-mentioned technical problem:
(1) to reach to examine and beat integrated unmanned plane and can carry out pursuit path and strike path according to obtained data are scouted
Independently select and realize independently to manipulate the effect that weapon module hits target in range, examine and make integrated unmanned plane machine
Carried data processing system must be able to airborne each reconnaissance module (visible light camera, laser ranging, synthetic aperture radar and irradiation
Photoelectric nacelle etc.) obtained data carry out real-time collecting, integration and target identification, by environmental variance locating for itself and unmanned plane
It imports the mission planning module in data processing system in real time in the form of task restriction, formulates current optimal target following and detect
Examine path and strike path.
The maximum technological difficulties of the technical problem are that more reconnaissances in data processing system integrate the design of module
With the design of mission planning module, scouting and in real time strike are followed to target which dictates that can realize with optimal path.It should
The solution of technological difficulties can not only promote height independence to examine the design and development for beating integrated unmanned plane, while also can be right
The design of the unmanned mechanized equipment of same type independence (unmanned vehicle, civilian unmanned plane and deep space exploration unmanned probing device etc.) plays
Facilitation.
(2) it to realize to the quick precision strike effect of target, need to improve long-range precise guidance and unmanned plane during flying control
The integrated technique of system.To realize that long-range precise guidance has to the guided missile for controlling unmanned plane transmitting with sufficiently high accuracy
Arrive at target position and after arriving at target proximity in maximum possible realization-handover of terminal guidance section.This technical problem
Key be that by the flight control system of missile brain and unmanned plane organically combine, to realize Long-range precision strike
With the effect of effective damage.
Summary of the invention
In view of the problems of the existing technology, the present invention provides a kind of scouting strike integration data processing system and sides
Method.
The invention is realized in this way integration data processing system, including technique preparation process mould are hit in a kind of scouting
Block and execution flow of task module；
Technique preparation process module includes unmanned plane and air weapon test, combustion oil filling, engine test etc.；
Executing flow of task module includes preparation stage, scouting and weapon preparation stage, transmitting before receiving an assignment and flying
Control and phase of the attack, make a return voyage and land after maintenance phase.
Another object of the present invention is to provide a kind of scouting hit integrated data processing method, specifically include following
Step:
Step 1: high speed scouts the integrated unmanned plane of strike, is located at immediately ahead of unmanned plane according to target when strike, calculates and divides
Analysis unmanned plane executes the various parameters of strike task under the conditions of different flying heights, flying speed；
Step 2: visible light camera/laser ranging/irradiation photoelectric nacelle is loaded with high-speed unmanned aerial vehicle, during strike
Target is scouted, is positioned and target illumination, covering hits process with the scouting for meeting target, realizes strike on a surface target
Precision；
Step 3: when implementing strike on a surface target, integrated unmanned plane carry precision guided weapon is hit for scouting, is needed
The booting of air weapon target seeker is wanted to capture target, terminal guidance hands over to the next shift in realization.
Further, in step 1, the various parameters of strike task are executed, horizontal distance, identification water including finding target
Flat distance, discovery to recognition time recognize needed for horizontal distance when locking required distance, arm discharge away from target, weapon
Underriding angle, after strike unmanned plane fly over photoelectricity ball after target can follow after horizontal distance, arm discharge photoelectricity ball persistently with
After track distance, transmitting can irradiation time and unmanned plane look over so as to check angular speed needed for photoelectricity ball needs to track target when putting on sky.
Further, it in step 1, is calculated as being calculated by the geometrical relationship of right angled triangle.
Further, in step 3, after completion is handed over to the next shift, attack precision depends on the end system of pointing accuracy and air weapon
Lead precision.
In conclusion advantages of the present invention and good effect are as follows:
The present invention carries out the key parameter that missile-borne unmanned plane executes during scouting the integrated task of strike and calculates analysis, realizes
Target location algorithm design, position error distribution and attack precision analysis, realize the data scouted and hit integrated unmanned plane
Processing system and method examine dozen integrated task for the execution of missile-borne unmanned plane and provide one from environmental data is obtained to formation task
The active path of instruction.
Disclosed in this invention data processing system using convenient and accurately calculation enough, rapidly and accurately converge
Always, multiple reconnaissance platforms mass data obtained is merged, calculated and analyzed, and combines the scouting to target fixed on this basis
Position data automatically generate the different paths for executing strike task, and filter out blow efficiency highest, institute by every constraint condition
The highest strike path of the most short and safety that takes time；Secondly, during carrying out strike task, the moment to dbjective state into
Row scouts positioning, and according to the state of airborne precision guided weapon and the progress path to be struck target, real-time to strike path
Be modified, and when guided weapon arrives at target proximity, with degree of precision realize in-final guidance hands over to the next shift, expected from realization
Attack precision.
Examining in the present invention, which is beaten integrated Unmanned Aerial Vehicle Data processing system and can be effectively improved, scouts during strike task
Every key parameter precision, thus substantially increase unmanned plane scouting precision and airborne precision guided weapon strike essence
Degree improves to examine and beats integrated unmanned plane for the high-speed maneuver of target, accurate navigator fix, long-range strike and accurately injure energy
Power enhances my strategfic reconnaissance, attack and land-sea aviation integral defence capability of army's existing weaponry and equipment in future war.
Detailed description of the invention
Fig. 1 is scouting strike integration data processing system block diagram provided in an embodiment of the present invention.
Fig. 2 is scouting strike integrated data processing method flow chart provided in an embodiment of the present invention.
Fig. 3 is that integrated unmanned plane execution mission flow diagram is hit in scouting provided in an embodiment of the present invention.
In figure: 1, preparing process module；2, flow of task module is executed.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to embodiments, to the present invention
It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to
Limit the present invention.
Application principle of the invention is described in detail with reference to the accompanying drawing；
As shown in Figure 1, integration data processing system, including technique preparation stream are hit in scouting provided in an embodiment of the present invention
Journey module 1 and execution flow of task module 2；
Technique preparation process module 1 includes unmanned plane and air weapon test, combustion oil filling, engine test etc.；
Executing flow of task module 2 includes preparation stage, scouting and weapon preparation stage, transmitting before receiving an assignment and flying
Control and phase of the attack, make a return voyage and land after maintenance phase.
As shown in Fig. 2, integrated data processing method is hit in scouting provided in an embodiment of the present invention, following step is specifically included
It is rapid:
S101: high speed, which is scouted, hits integrated unmanned plane, is located at immediately ahead of unmanned plane according to target when strike, calculates and analyze
Unmanned plane executes the various parameters of strike task under the conditions of different flying heights, flying speed；
S102: loading visible light camera/laser ranging/irradiation photoelectric nacelle with high-speed unmanned aerial vehicle, right during strike
Target scouted, position and target illumination, covering hit process with the scouting for meeting target, realizes strike essence on a surface target
Degree；
S103: when implementing strike on a surface target, integrated unmanned plane carry precision guided weapon is hit for scouting, is needed
The booting of air weapon target seeker captures target, and terminal guidance hands over to the next shift in realization.
In step S101, the various parameters provided in an embodiment of the present invention for executing strike task, the water including finding target
Flat distance, discovery to recognition time, recognizes the level away from target when locking required distance, arm discharge at identification horizontal distance
Unmanned plane is flown over after photoelectricity ball after target can follow horizontal distance, arm discharge after distance, underriding angle, strike needed for weapon
Photoelectricity ball continue after tracking range, transmitting can irradiation time and unmanned plane photoelectricity ball when putting on sky of looking over so as to check need needed for tracking target
Angular speed.
It is provided in an embodiment of the present invention to be calculated as being calculated by the geometrical relationship of right angled triangle in step S102.
In step S103, it is provided in an embodiment of the present invention completion hand over to the next shift after, attack precision depend on pointing accuracy and
The terminal guidance precision of air weapon.
Application principle of the invention is further described combined with specific embodiments below；
Scouting and hitting integrated UAV system workflow includes technique preparation process and execution flow of task.Technique preparation
Process includes unmanned plane and air weapon test, combustion oil filling, engine test etc.；Executing flow of task includes receiving an assignment
And preparation stage, scouting and weapon preparation stage, emission control and phase of the attack before flying, make a return voyage and land after maintenance phase.
As shown in figure 3, integrated unmanned plane is hit in scouting provided in an embodiment of the present invention executes mission flow diagram.
It is sharp to load Visible Light Reconnaissance/Target indication equipment (photoelectric nacelle), carry that high speed scouts the integrated unmanned plane of strike
Light guide bomb is Typical Disposition, is located at immediately ahead of unmanned plane according to target when strike, calculates and analyzes unmanned plane different winged
Row height, the various parameters that strike task is executed under the conditions of flying speed, including find the horizontal distance of target, identification it is horizontal away from
From, discovery to recognition time, recognize lock required distance, arm discharge when horizontal distance away from target, bow needed for weapon
After angle of attack degree, strike unmanned plane fly over photoelectricity ball after target can follow after horizontal distance, arm discharge photoelectricity ball persistently track away from
From after, transmitting can irradiation time and unmanned plane look over so as to check angular speed needed for photoelectricity ball needs to track target when putting on sky etc., these
Process is calculated by the geometrical relationship of right angled triangle.Attack precision analysis on a surface target is loaded with high-speed unmanned aerial vehicle
Visible light camera/laser ranging/irradiation photoelectric nacelle uses the machine to be scouted, positioned to target and mesh during strike
Mark irradiation, which, which can cover, hits process to the scouting for meeting target.When implementing strike on a surface target, strike essence is influenced
The link of degree includes to target positioning, air weapon midcourse guidance and terminal guidance is relieved and the links such as Target indication.For scouting
Integrated unmanned plane carry precision guided weapon is hit, target location accuracy influences the midcourse guidance process of air weapon, needs airborne
After the booting of weapon target seeker, target can be captured, terminal guidance hands over to the next shift in realization.After completion is handed over to the next shift, attack precision is depended on
The terminal guidance precision of pointing accuracy and air weapon.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (5)
1. integration data processing system is hit in a kind of scouting, which is characterized in that the scouting strike integration data processing
System, including technique preparation process module and execution flow of task module；
Technique preparation process module includes unmanned plane and air weapon test, combustion oil filling, engine test etc.；
Executing flow of task module includes preparation stage, scouting and weapon preparation stage, emission control before receiving an assignment and flying
And phase of the attack, make a return voyage and land after maintenance phase.
2. integrated data processing method is hit in a kind of scouting, which is characterized in that the scouting strike integration data processing
Method, specifically includes the following steps:
Step 1: high speed, which is scouted, hits integrated unmanned plane, is located at immediately ahead of unmanned plane according to target when strike, calculates and analyze nothing
The man-machine various parameters that strike task is executed under the conditions of different flying heights, flying speed；
Step 2: visible light camera/laser ranging/irradiation photoelectric nacelle is loaded with high-speed unmanned aerial vehicle, to mesh during strike
Mark is scouted, is positioned and target illumination, and covering hits process with the scouting for meeting target, realizes strike essence on a surface target
Degree；
Step 3: when implementing strike on a surface target, integrated unmanned plane carry precision guided weapon, airborne force are hit for scouting
Target is captured after the booting of device target seeker, terminal guidance hands over to the next shift in realization.
3. as claimed in claim 2 scout strike integrated data processing method, which is characterized in that in the step 1, hold
The various parameters of row strike task, horizontal distance, identification horizontal distance, discovery to recognition time, identification including finding target
Horizontal distance away from target when to locking required distance, arm discharge, unmanned plane is flown over after underriding angle, strike needed for weapon
Photoelectricity ball can follow photoelectricity ball after horizontal distance, arm discharge can irradiation time and nothing after continuing tracking range, transmitting after target
Man-machine angular speed needed for photoelectricity ball needs to track target when putting on sky of looking over so as to check.
4. as claimed in claim 2 scout strike integrated data processing method, which is characterized in that in the step 1, lead to
The geometrical relationship for crossing right angled triangle is calculated.
5. as claimed in claim 2 scout strike integrated data processing method, which is characterized in that complete in the step 3
After handing over to the next shift, attack precision depends on the terminal guidance precision of pointing accuracy and air weapon.
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| CN110596698A (en) * | 2019-07-25 | 2019-12-20 | 姚碧琛 | Active and passive integrated unmanned aerial vehicle detection and identification technology |
| CN111781955A (en) * | 2020-06-15 | 2020-10-16 | 北京理工大学 | Aircraft laser guidance control system and method provided with piloting helicopter |
| CN112256053A (en) * | 2020-09-27 | 2021-01-22 | 中国航空工业集团公司洛阳电光设备研究所 | Fire control photoelectric system of small-sized scouting and fighting unmanned aerial vehicle |
| CN112327927A (en) * | 2020-11-25 | 2021-02-05 | 北京理工大学 | Multi-angle strike track planning method for formation unmanned aerial vehicles based on grid planning algorithm |
| CN112395543A (en) * | 2020-10-12 | 2021-02-23 | 中国兵器科学研究院 | Equipment system reconnaissance capability assessment method, device, equipment and medium |
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| CN113093601A (en) * | 2021-03-30 | 2021-07-09 | 中琪华安(北京)科技有限公司 | Close-range aviation firepower support system and method |
| CN113985926A (en) * | 2021-10-22 | 2022-01-28 | 航天科工通信技术研究院有限责任公司 | Unmanned aerial vehicle guidance missile attack system |
| CN114604424A (en) * | 2020-12-09 | 2022-06-10 | 北京理工大学 | Patrol, flight, check and fight integrated platform |
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| CN114604424A (en) * | 2020-12-09 | 2022-06-10 | 北京理工大学 | Patrol, flight, check and fight integrated platform |
| CN112781449A (en) * | 2020-12-22 | 2021-05-11 | 北京航天飞腾装备技术有限责任公司 | Combat application method and device of laser guided weapon |
| CN113093601A (en) * | 2021-03-30 | 2021-07-09 | 中琪华安(北京)科技有限公司 | Close-range aviation firepower support system and method |
| CN113985926A (en) * | 2021-10-22 | 2022-01-28 | 航天科工通信技术研究院有限责任公司 | Unmanned aerial vehicle guidance missile attack system |
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