阅读说明：本技术 一种低空飞行器指挥控制系统 (Low-altitude aircraft command control system ) 是由 徐凡 王军 冯希旺 张天华 张洋 翟俊杰 黄建伟 刘彬 于 2019-09-03 设计创作，主要内容包括：一种低空飞行器指挥控制系统,由服务模块、安全及权限管理模块两大部分组成,通过数据交互管理在数据库中植入信息融合算法的模型、战术布设的模型、武器效能分析模型,将采集的低空飞行器相关数据通过这些建立的模型进行分析,并将分析的结论通过电信号传输给管理平台,通过多个多种传感器实施数据的收据,并通过信号传导端口接受和输出电信号,从而控制组合多种处置打击无人飞行器的手段,同时对重点区域进行划分,设立禁飞区、安全区、飞行任务区、飞行走廊等管制区,在特定区域内管理备案无人飞行器的飞行计划和任务时,同时加强该区域的管制能力,具备识别敌我无人飞行器的能力和处置威胁无人飞行器的功能。(A command control system of a low-altitude aircraft comprises a service module and a safety and authority management module, implanting a model of an information fusion algorithm, a model of tactical layout and a weapon efficiency analysis model in a database through data interaction management, analyzing the collected related data of the low-altitude aircraft through the established models, transmitting the analyzed conclusion to a management platform through an electric signal, data receipt is effected by a plurality of various sensors, and electrical signals are received and output through signal conducting ports, thereby controlling and combining various means for disposing and striking the unmanned aerial vehicle, dividing key areas, setting control areas such as a no-fly area, a safety area, a flight mission area, a flight corridor and the like, when the flight plan and the tasks of the unmanned aerial vehicle are recorded in a specific area, the control capacity of the area is enhanced, and the unmanned aerial vehicle has the capacity of identifying the enemy unmanned aerial vehicle and the function of disposing threat unmanned aerial vehicle.)

1. A low-altitude aircraft command and control system is characterized in that: the system comprises a service module and a security and authority management module, wherein the service module has the functions of application management and comprises the functions of situation display, auxiliary decision, system management and equipment management, and equipment managed by the equipment is communication equipment and equipment with a man-machine conversation function; the safety and authority management module has the functions of man-machine interaction management, data interaction management and basic equipment management, the human-computer interaction management is that the conclusion of data interaction management analysis is displayed to the staff through the management platform, the staff gives specific instructions through the management platform, the data interaction management is to implant a model of an information fusion algorithm, a model of tactical layout and a weapon efficiency analysis model in a database, analyze the collected related data of the low-altitude aircraft through the established models, and transmitting the analyzed conclusion to a management platform through electric signals, wherein the basic equipment management is the management aiming at a server, network security, an operating system and a signal transmission port, the signal transmission ports are two types and are respectively an input port and an output port, the input port is used for receiving signals, and the output port is used for sending signals; the management platform is connected with a plurality of sensors, input ports, a treatment striking means, communication equipment and equipment with a man-machine conversation function; the sensor comprises a radar and a passive detection, and the treatment and striking means comprises electromagnetic suppression, a laser weapon and a net capture device;

The situation display takes a map as a bottom layer, and an area planning layer, a grid defense layer, a key target layer, a threat target layer, a predetermined flight plan route layer and a local arrangement layer are respectively added;

The region planning layer is used for planning a flight corridor, a take-off and landing area and a no-fly area, the flight corridor is planned in an airspace management and flight task and specifically sets a flight direction, a flight height and a flight time, the flight corridor is arranged above a safety area and is an air channel with the width of 100 meters, the take-off and landing area is an area for taking off and landing of a documented unmanned aerial vehicle, a circular area with the radius of 10 meters is used, and the no-fly area is an area which is not allowed to fly;

The grid defense layer is formed by dividing warps and wefts on a situation display map, wherein the wefts are represented by English letters, the warps are represented by Arabic numerals, and blocks needing protection are divided by grids for protecting the grids. The key target layer is used for identifying key target areas in a situation display map;

the threat target layer is used for generating a track of the unmanned aerial vehicle in a situation display map and marking the information of the target such as batch, height, speed, azimuth angle and track ID;

the flight planning route layer is used for generating track information of the recorded unmanned aerial vehicle in a situation display map according to time and marking information of target batches, heights, speeds, azimuth angles, track IDs, flight units, flight time, flight purposes and track areas;

The local arrangement layer is an area acting on the treatment equipment, the area is also an action area of sensors such as radar and photoelectric sensors, and weapon equipment is arranged in the area.

2. the low-altitude aircraft command and control system according to claim 1, wherein: the communication equipment can be set to a multi-equipment communication mode, and can also monitor the connection state and the data transmission state of the equipment, and meanwhile, the communication port can realize monitoring and data packet preprocessing.

Technical Field

the invention relates to the field of low-altitude aircraft management control, in particular to a command control system of a low-altitude aircraft.

background

At present, various traditional anti-unmanned aerial vehicle systems emerge at home and abroad, and a mode of combining a single sensor and a single treatment striking means is mainly adopted to search, track and strike low-altitude flight targets in key areas; the prior art has no instruction control system or only a simple instruction control system, and has the following defects:

1. A plurality of sensors and information input interfaces cannot be managed, only warning search can be carried out through a single sensor, the discovery probability is low, the target tracking is discontinuous, and the loss rate is high;

2. The low-altitude unmanned aerial vehicle with threat cannot be hit by multiple disposal means, the target can be hit only by a single means, the capture rate is low, and the hitting effect is poor;

3. The low-altitude airspace division of the key point area cannot be accurately carried out, and control areas such as a no-fly area, a safety area, a flight mission area, a flight corridor and the like are set, so that the airspace with special requirements cannot be effectively controlled;

4. the basic flight situation of a given target cannot be effectively managed;

5. the enemy low-altitude aircraft cannot be effectively identified, and the adoption of the hitting means can cause misjudgment and accidental injury to the low-altitude aircraft of the party.

Disclosure of Invention

The invention provides a command control system of a low-altitude aircraft, which aims to solve the problems in the prior art and provide a command control system capable of effectively defending, managing and disposing the low-altitude aircraft in a given area.

the technical scheme adopted by the invention for solving the problems is as follows:

A low-altitude aircraft command and control system is characterized in that: the system comprises a service module and a security and authority management module, wherein the service module has the functions of application management and comprises the functions of situation display, auxiliary decision, system management and equipment management, and equipment managed by the equipment is communication equipment and equipment with a man-machine conversation function; the safety and authority management module has the functions of man-machine interaction management, data interaction management and basic equipment management, the human-computer interaction management is that the conclusion of data interaction management analysis is displayed to the staff through the management platform, the staff gives specific instructions through the management platform, the data interaction management is to implant a model of an information fusion algorithm, a model of tactical layout and a weapon efficiency analysis model in a database, analyze the collected related data of the low-altitude aircraft through the established models, and transmitting the analyzed conclusion to a management platform through electric signals, wherein the basic equipment management is the management aiming at a server, network security, an operating system and a signal transmission port, the signal transmission ports are two types and are respectively an input port and an output port, the input port is used for receiving signals, and the output port is used for sending signals; the management platform is connected with a plurality of sensors, input ports, a treatment striking means, communication equipment and equipment with a man-machine conversation function; the sensor comprises a radar and a passive detection, and the treatment and striking means comprises electromagnetic suppression, a laser weapon and a net capture device;

The situation display takes a map as a bottom layer, and an area planning layer, a grid defense layer, a key target layer, a threat target layer, a predetermined flight plan route layer and a local arrangement layer are respectively added;

the region planning layer is used for planning a flight corridor, a take-off and landing area and a no-fly area, the flight corridor is planned in an airspace management and flight task and specifically sets a flight direction, a flight height and a flight time, the flight corridor is arranged above a safety area and is an air channel with the width of 100 meters, the take-off and landing area is an area for taking off and landing of a documented unmanned aerial vehicle, a circular area with the radius of 10 meters is used, and the no-fly area is an area which is not allowed to fly;

the grid defense layer is formed by dividing warps and wefts on a situation display map, wherein the wefts are represented by English letters, the warps are represented by Arabic numerals, and blocks needing protection are divided by grids for protecting the grids. The key target layer is used for identifying key target areas in a situation display map;

the threat target layer is used for generating a track of the unmanned aerial vehicle in a situation display map and marking the information of the target such as batch, height, speed, azimuth angle and track ID;

The flight planning route layer is used for generating track information of the recorded unmanned aerial vehicle in a situation display map according to time and marking information of target batches, heights, speeds, azimuth angles, track IDs, flight units, flight time, flight purposes and track areas;

The local arrangement layer is an area acting on the treatment equipment, the area is also an action area of sensors such as radar and photoelectric sensors, and weapon equipment is arranged in the area.

the communication equipment can be set to a multi-equipment communication mode, and can also monitor the connection state and the data transmission state of the equipment, and meanwhile, the communication port can realize monitoring and data packet preprocessing.

The invention has the beneficial effects that: the receipt of data is implemented through a plurality of sensors, and electric signals are received and output through the signal conduction port, so that a plurality of measures for dealing with and striking the unmanned aerial vehicle are controlled and combined, meanwhile, key areas are divided, control areas such as a no-fly area, a safety area, a flight mission area and a flight corridor are set up, when the flight plan and mission of the unmanned aerial vehicle are managed and recorded in a specific area, the control capacity of the area is enhanced, and the unmanned aerial vehicle safety system has the capacity of identifying the enemy unmanned aerial vehicle and the function of dealing with and threatening the unmanned aerial vehicle.

Drawings

FIG. 1 is a schematic diagram of the architecture of the system of the present invention.

Detailed Description

the invention is further described below with reference to the accompanying drawings and specific examples.

As shown in fig. 1, the command and control system for a low-altitude aircraft comprises a service module and a security and authority management module, wherein the service module has functions of application management, including functions of situation display, aid decision, system management and equipment management, and the equipment for equipment management is communication equipment and equipment with a man-machine conversation function; the safety and authority management module has the functions of man-machine interaction management, data interaction management and basic equipment management, the human-computer interaction management is that the conclusion of data interaction management analysis is displayed to the staff through the management platform, the staff gives specific instructions through the management platform, the data interaction management is to implant a model of an information fusion algorithm, a model of tactical layout and a weapon efficiency analysis model in a database, analyze the collected related data of the low-altitude aircraft through the established models, and transmitting the analyzed conclusion to a management platform through electric signals, wherein the basic equipment management is the management aiming at a server, network security, an operating system and a signal transmission port, the signal transmission ports are two types and are respectively an input port and an output port, the input port is used for receiving signals, and the output port is used for sending signals; the management platform is connected with a plurality of sensors, input ports, a treatment striking means, communication equipment and equipment with a man-machine conversation function; the sensor comprises a radar and a passive detection, and the treatment and striking means comprises electromagnetic suppression, a laser weapon and a net capture device; the model of the information fusion algorithm is characterized in that multi-platform information is cooperatively utilized, information provided by each platform is unified to the same platform for analysis, traces are correlated, the advantage of multi-platform multi-radar data fusion is exerted to the maximum extent, and time alignment and space alignment are carried out by using correlated results, namely space-time alignment of data; the time alignment is to calculate data information of the target at other moments by using the measurement data of the same target, correlate the collected trace point data to the measurement data of a certain sensor, find out the measurement data of the same target in different scanning periods, determine the general position of the target in the next scanning period by using the motion characteristics of the target, the position information of the current point of the target and the scanning period of the sensor, and obtain the position range of the target in the next scanning period by using the rough correlation of the positions, namely, the rough correlation of the positions is to use the above information to obtain the position range of the target in the next scanning period; after the positions are correlated, for the condition that a plurality of points exist in the annular correlation gate, further confirmation is needed, the positions cannot be accurately determined, and judgment needs to be carried out in consideration of the storage time. Regarding time correlation, the information of the scanning period is fully utilized to analyze and judge the data in the circular ring; the time difference between two adjacent periodic measurement points from the same target is the period of the radar scan plus a small value Δ r, and is given by the formula: x (nT +1) -X (nT) -T +. DELTA.r, wherein X (nT) represents the measurement time of one measurement data of the radar in a certain scanning period, and X (nT + I) represents the measurement time of one point in the circular ring obtained by position coarse correlation of the measurement data in the next scanning period, wherein the measurement time refers to the time when the sensor acquires the measurement point. The delta r can be positive or negative, and the delta r is a positive description target; the motion direction is consistent with the direction of the radar line buckling and is opposite to the direction of the negative explanation, a point with the time difference with the measured data closest to the radar scanning period is selected in a circular ring and used as the point of the measured data of the target in the next scanning period, when fusion estimation is carried out, the point from the same target at the same moment needs to be found out, only then, the points can be subjected to fusion operation, the fusion center of the points is found out, and the point-trace correlation is needed to realize the fusion estimation; obtaining a position point of a certain target at a certain moment on a fusion center platform through estimation, setting a proper correlation gate around the point in data converted from the measurement values of all sensors, finding out the points from the target at the moment, setting a circular wave gate by taking the position point as the center of a circle, fusing the points in the correlation gate by taking the circular wave gate as the correlation gate, and calculating a fusion center;

the evaluation of the weapon performance is related to technical and tactical indexes of weapon equipment, and n technical and tactical indexes Pi are (P1, P2, …, Pn); the performance function F ═ F (K1P1+ … + KnPn), where K is the weighting factor for each index, the weighting factors are mainly calculated empirically,

The situation display takes a map as a bottom layer, and an area planning layer, a grid defense layer, a key target layer, a threat target layer, a predetermined flight plan route layer and a local arrangement layer are respectively added;

the region planning layer is used for planning a flight corridor, a take-off and landing area and a no-fly area, the flight corridor is planned in an airspace management and flight task and specifically sets a flight direction, a flight height and a flight time, the flight corridor is arranged above a safety area and is an air channel with the width of 100 meters, the take-off and landing area is an area for taking off and landing of a documented unmanned aerial vehicle, a circular area with the radius of 10 meters is used, and the no-fly area is an area which is not allowed to fly;

The grid defense layer is formed by dividing warps and wefts on a situation display map, wherein the wefts are represented by English letters, the warps are represented by Arabic numerals, and blocks needing protection are divided by grids for protecting the grids. The key target layer is used for identifying key target areas in a situation display map;

the threat target layer is used for generating a track of the unmanned aerial vehicle in a situation display map and marking the information of the target such as batch, height, speed, azimuth angle and track ID;

The flight planning route layer is used for generating track information of the recorded unmanned aerial vehicle in a situation display map according to time and marking information of target batches, heights, speeds, azimuth angles, track IDs, flight units, flight time, flight purposes and track areas;

the local arrangement layer is an area acting on the treatment equipment, the area is also an action area of sensors such as radar and photoelectric sensors, and weapon equipment is arranged in the area.

The communication equipment can be set to a multi-equipment communication mode, and can also monitor the connection state and the data transmission state of the equipment, and meanwhile, the communication port can realize monitoring and data packet preprocessing.

The receipt of data is implemented through a plurality of sensors, and electric signals are received and output through the signal conduction port, so that a plurality of measures for dealing with and striking the unmanned aerial vehicle are controlled and combined, meanwhile, key areas are divided, control areas such as a no-fly area, a safety area, a flight mission area and a flight corridor are set up, when the flight plan and mission of the unmanned aerial vehicle are managed and recorded in a specific area, the control capacity of the area is enhanced, and the unmanned aerial vehicle safety system has the capacity of identifying the enemy unmanned aerial vehicle and the function of dealing with and threatening the unmanned aerial vehicle.

The invention forms the low-altitude air-space control capability of the key point region by means of low-altitude control and defense strategies combined by management, air-space division, friend-foe identification, flight mission comparison, deviation region alarm and the like of a command control system. The multi-sensor searching, tracking and locking are controlled through the command control system, tactical analysis is carried out, various striking means are adopted, effective striking is carried out on a threat target, and the combination of various sensors and the striking means can improve the finding and tracking capability and the capturing capability to the greatest extent.

various input ports (the combination of the input ports is? how to set the ports), and the information of the added empty condition is provided, so that search and discovery means are enriched and improved;

The command control system can improve situation perception capability through image detection and monitoring of a take-off area, a flight area and a control area;

the command control system can select the most effective striking means for treatment through tactical analysis and efficiency study and judgment, thereby improving the treatment efficiency.

the command control system can set different airspaces and take-off areas, monitor the take-off areas in real time, manage unmanned planes of the same party, plan flight corridors and confirm the targets again by the inspection points. And (4) comparing the targets found in different airspaces with the flight mission, warning the targets in the deviated area, and disposing the threat targets.

The unmanned aerial vehicle flying for recording in a specific area has the advantages that information of the overhead takeoff time, the flight time, the landing time, the flight height, the flight track, the flight purpose, the flight unit, the contact way and the like of flying is reported in advance during recording, the data of a found target and the data reported in advance are compared through a radar to indirectly judge and identify the enemy, once flight deviation occurs, the unmanned aerial vehicle can be communicated with related flying officers through communication equipment to adjust a flight route, if the deviation continues after warning, warning is given out through the communication equipment, and the unmanned aerial vehicle is subjected to force attack after the warning is invalid.

the force striking means mainly comprises:

1. the target may be dislodged using an electromagnetic suppression system;

2. Using a GPS decoy system to decoy and land the target to a specified place;

3. physically damaging the target using a laser weapon;

4. and capturing the target by using the capturing device.